EA022170B1 - Battery system for a vehicle with severable connections - Google Patents

Abstract

A battery system for storing electrical power and supplying electrical power to a vehicle is provided. The system includes multiple battery packs, and each battery pack includes a plurality of cells. The cells in each battery pack are electrically connected with one another and the multiple battery packs are also electrically connected with one another to combine the total energy output of the cells of the system. The electrical connections between at least some of the cells include a severable feature, whereby the electrical connection is severed locally at the severable feature(800a, 800b) in response to an impact force that is in excess of a predetermined magnitude and/or an overcurrent/overtemperature condition.

Description

Technical field

The present invention is directed to battery cells and battery devices, and more particularly to lithium-ion battery cells and battery devices that can be used in vehicles, such as an electric vehicle and / or hybrid vehicle, having an electric motor.

State of the art

Rechargeable batteries, such as lithium-ion polymer batteries, have a wide range of applications. Applications include, for example, laptop batteries, cell phone batteries, and power supplies for other personal electronic devices. These devices require lightweight batteries with moderate power output. However, lithium-ion polymer batteries are also capable of providing power to devices for which a significantly higher output power is required than for the personal electronic devices mentioned above. For example, lithium-ion polymer batteries with high power output can be used to power industrial equipment, high power communications, vehicles, and the like. The use of lithium-ion polymer battery devices with high power output can be especially important in the field of driving vehicles.

The public is becoming increasingly sensitive to the cost of fossil fuels and environmental problems associated with its use. One of the problems is the exhaust fumes of vehicles burning fossil fuels, and the corresponding environmental pollution.

Alternatives to such vehicles include electric vehicles that are driven exclusively by electric motors, and hybrid vehicles that use both electric and fossil fuel engines. These alternatives are likely to play an increasingly important role as a replacement for modern vehicles.

Although consumers are attracted to the benefits of pure electric and hybrid cars related to pollution control, they want cars with electric motors that share the same characteristics as their fossil fuel counterparts. To achieve these goals, problems related to battery performance and reliability must be resolved. For this, lithium-ion batteries are preferred over other more conventional types of batteries. Lithium-ion batteries are applicable for this purpose, since they have a high specific energy, which reduces the amount of space occupied by the battery in the vehicle. In addition, they can be designed to weigh less than conventional batteries.

- 1 022170

Battery devices for use with electric motors used in purely electric and hybrid vehicles do not currently meet the necessary requirements in many ways. The individual battery cells of a battery device are often heavy, bulky, and unreliable. In addition, the battery cells are not currently designed and not applicable in order to effectively provide the high output power required to accelerate the vehicle at a suitable acceleration level. In addition, the electrochemistry, the core structures of the cells, electrical interconnections and shell structures, which are often unreliable, dangerous and generally unsuitable for use in electric vehicles, are used in individual battery cells.

In order to overcome the power deficit associated with individual battery cells, attempts were made to connect several individual battery cells to one another so that their combined output power provided the required drive power. Interconnections between the individual battery cells, on the other hand, are often unreliable. In addition, not enough has been done to ensure the reliability of such multi-cell battery devices. Not properly directed efforts to prevent short circuits, as well as explosions. High output power batteries should be designed so that efforts are focused on aspects such as performance, service life, reliability and safety, if they are suitable for the large number of applications in which such batteries can be used. devices.

SUMMARY OF THE INVENTION

A battery device for storing electric power and supplying electric power to a vehicle is disclosed. The device includes many rechargeable batteries, each with many elements. The cells in each battery are electrically connected to one another, and the plurality of batteries are also electrically connected to one another to combine the total generated energy of the elements of the device. Electrical connections between at least some elements include a splittable feature, whereby the electrical connection is locally split on that splittable feature in response to an impact force that exceeds a predetermined amount and / or an over current / over temperature condition.

Brief Description of the Drawings

The invention may be better understood by reference to the following drawings and description. The components in the figures are not necessarily represented to scale, and instead, emphasis is placed on illustrating the principles of the present invention. In addition, in the figures, the same numerals denote corresponding parts in all different views.

FIG. 1 is a cross-sectional view of a typical multilayer battery sheet that can be used to form a wound core of a battery cell.

FIG. 2A is a perspective view of a tapered core roll used in a battery cell.

FIG. 2Β-2Ό show an alternative embodiment of the core, in which the sheets forming the core are not wound.

FIG. 3 is a perspective view of the anode end of a battery cell 300 having a wound core of FIG. 2A.

FIG. 4 is a schematic cross-sectional view of a battery cell 300.

FIG. 5 and 6 illustrate one method for forming regions of the anode sheet and / or cathode sheet that abut against open substrates.

FIG. 7 is a cross-sectional view of one example of a wound core.

FIG. 8 shows one embodiment of a brittle bent connector.

FIG. 9 shows another embodiment of a brittle bent connector.

FIG. 10 shows how the bent connector of FIG. 8 can be used to interconnect adjacent battery cells.

FIG. 11 shows another structure for interconnecting adjacent battery cells.

FIG. 12 and 13 show a connecting structure that can be used to bring the core of a battery cell to an optimum operating temperature.

FIG. 14A shows one of the methods for connecting several cores of a battery cell with a curved connector of FIG. 8.

FIG. 14Β shows one method of connecting a structure to a single core

- 2 022170 battery cells with a curved connector of FIG. 8.

FIG. 15 is a plan view of a gasket applied at each end of a containment shell of a battery cell.

FIG. 16 and 17 show one method of sealing the end of the containment that surrounds the wound core around the periphery.

FIG. 18-20 show one embodiment of a blown assembly that can be used on the end cap assembly of a battery cell.

FIG. 21 and 22 show alternative pressure relief structures that can be used to supplement and / or replace the blower assembly shown in FIG. eighteen.

FIG. 23 is a structural diagram of a battery in which multiple battery cells are connected to one another and grouped within one housing.

FIG. 24-26 illustrate one embodiment of a housing that can be used to form a battery.

FIG. 27 shows a connector that can be used to mechanically and electrically connect adjacent batteries.

FIG. 28 shows how the connector of FIG. 27.

FIG. 29 shows a battery device that supplies electric power to an engine / generator and receives electric power from an engine / generator of a vehicle capable of being driven by electric power.

FIG. 30-34 illustrate the benefits of providing connections to the anode and cathode of a wound core at opposite ends of the core.

FIG. 35-41 illustrate other structures for interconnecting battery cells.

FIG. 41A illustrates a brittle joint structure having a thermally activated detachable clip.

FIG. 42-46 illustrate interconnection patterns of battery cells in which terminals of battery cells are connected to one another by a bridge connector.

FIG. 47 and 48 illustrate interconnection patterns of battery cells having current protection substructures using gravity.

FIG. 49-51 illustrate the interconnection patterns of the battery cells having thermal expansion parameters such that the terminals of the battery cells are separated under conditions of excessive current.

FIG. 52 and 53 illustrate interconnecting battery cells having overcurrent protection substructures based on a chemical interaction between a chemical released by the substructure and one or more terminal / interconnecting portions of the battery cell interconnections.

FIG. 54-60 illustrate interconnection patterns of battery cells having substructures for protection against excessive currents based on electrical connections / disconnections provided by the presence / absence of a liquid conductor.

FIG. 61-64 illustrate various embodiments of a protective cover for the end cap assembly of a battery cell.

FIG. 65-67 illustrate another embodiment of a blow hole.

FIG. 68 shows another embodiment of a connector that can be used to mechanically and electrical interconnect adjacent batteries.

FIG. 69 shows how the connectors of FIG. 27 and 68 can be applied when the batteries are arranged in a transverse arrangement.

Detailed Description of Preferred Embodiments

Lithium-ion polymer batteries are a type of rechargeable battery in which lithium ions move between the anode and cathode. Lithium ions move from anode to cathode during discharge and from cathode to anode during charging.

FIG. 1 is a cross-sectional view of a typical laminated battery sheet 100 that can be wound to form a wound core of a battery cell. The battery sheet 100 of FIG. 1 includes three functional components: the anode sheet 105, the cathode sheet 110 and the separator sheet 115. The anode sheet 105 may include active anode layers 106 located on opposite sides of the anode substrate 107. The anode substrate 107 may be formed from one or more layers of metal foil, for example copper. Active anode layers 106 may be formed from graphite or other carbon based material. In one example, the active layers 106 of the anode sheet 105 can be made using 100 g of natural graphite with 3 g of polyvinylidene fluoride (RUER) as a binder and 3 g of acetylene black as a conductive agent added to 100 g of ΝΙ- methylpyrrolidone (ΝΜΡ). The components can be mixed in a vacuum mixer to form a homogeneous suspension. The suspension can be applied as a coating with a thickness of about 12 microns on each side of the substrate 107, for example, of copper foil, forming a structure having a composite layer with a thickness of about 100-110 microns. The coated foil can then be dried at a temperature of about 90 ° C, forming an anode 115.

The cathode sheet 110 may include active cathode layers 112 located on opposite sides of the cathode substrate 114. The cathode substrate 114 may be formed from one or more layers of a metal foil, such as aluminum. The active cathode layers 112 may be formed from materials such as layered oxide (e.g., lithium cobalt oxide), a polyanion based material (e.g., lithium-iron phosphate), or spinel (e.g., lithium-manganese oxide), although such materials like Τίδ ₂ (titanium disulfide) can also be used.

In one example, the active layers 112 of the cathode sheet 110 may be formed by combining at least one lithium metal compound with at least one mixed metal crystal, the metal crystal comprising a mixture of metal elements and metal oxides. The lithium compound can be an intercalation metal compound of the general formula iM ₍ ., C, XO _c . In which M is a first-order transition metal, such as Fe, Μη, Νί, V, Co and Τί; N is a metal selected from the group Fe, Μη, Νί, V, Co, Τί, Μ§, Ca, Cu, N6, Ζγ and rare-earth metals; X is selected from the elements P, δί, δ, V and Ce; and a, b and c have values that provide neutral charge of the intercalation metal compound The metal compound may have the general formula M _with H | - in which M is a metal selected from the groups ΙΑ, ΙΙΑ, ΙΙΙΑ, ίνΑ, νΑ, ΙΙΙΒ, ΐ νΒ and νΒ of the Periodic Table; N is selected from O, Ν, Η, δ, δθ ₄ , PO ₄ , OH, C1, P and C; and 0 <c <4 and 0 <b <6. In other examples, the metal compound may include one or more components selected from the group consisting of MdO, διΌ, Α1 ₂ Ο ₃ , δηθ ₂ , δ% Ο ₃ , Υ ₂ Ο ₃ , ΤίΟ ₂ and ν ₂ Ο _5. The metal compound and lithium compound may be heated or sintered at about 600-900 ° C. under an inert gas or reducing gas atmosphere for about 2 hours to form material for the cathode sheet 110.

In another example, a metal compound can be formed as a mixed crystalline compound of the general formula Ε ^ Αμ ^ Β ^ ΧΟ ^ / Μ, Ν * in which A is a transition metal of the first row, including Fe, Μη, Νί, V, Co and Τί; B is a metal selected from the group Fe, Μη, Νί, V, Co, Τί, Μ§, Ca, Cu, ΝΕ Ζγ and rare earth metals; X is selected from the elements P, δί, δ, V and Ce; Μ is a metal selected from the groups ΙΑ, ΙΙΑ, ΙΙΙΑ, ^ L, VΑ, ΙΙΙΒ, ΙΥΒ and \ B of the Periodic table; Ν is selected from O, Ν, Η, δ, δΟ ₄ , PO ₄ , OH, C1, P and C; and in which 0 <a <1, 0 <y <0.5, 0 <b <1, 0 <c <4 and 0 <| <6. Particle sizes may be less than about 10 microns, with a preferred size of 3-5 microns.

The active cathode material may include a first crystalline compound and a second crystalline compound. The first crystalline compound may be distributed within the second crystalline compound to form a complex compound. The first crystalline compound can be prepared by heating a combination of at least one lithium source, at least one iron source and at least one phosphate source, while the second crystalline compound can be prepared by heating at least two metal compounds. The second crystalline compound may also include one or more components selected from the groups ΙΑ, ΙΙΑ, ΙΙΙΑ, ^ Α, VΑ, ΙΙΙΒ, ΙΎΒ and \ B of the Periodic table.

During the formation of the cathode active material, a large number of crystal defects can be introduced into intermediate or complex crystals, so that the electronic states and the formation of metal oxides change. A metal compound with its mixed crystalline structure may therefore include a large number of oxygen vacancies and missing oxygen atoms. Oxygen vacancies can facilitate carrier transfer, thereby improving the electrical conductivity of the mixed crystal. To this end, the metal compound may have a smaller crystal lattice than the lithium compound, so that it can be received or distributed within the lithium compound. Alternatively, the metal compound may be received or distributed between two or more large crystal lattices. In addition, the metal compound may be located at the grain boundaries of the lithium compound. Finally, the metal compound can be dispersed on the outer surfaces of the grains of the lithium compound. In each case, the migration of lithium ions serves as a bridge either inside the crystal lattice or between two or more crystal lattices. Lithium ions can be completely released to improve electrical properties, including electrical conductivity, capacitance, and rechargeability.

Preferably, the metal compound can be distributed in the lithium-iron phosphate compound, forming a complex compound for use on the cathode sheet 110. The metal compound can be distributed within the lithium-iron phosphate compound, forming a mixed crystal. In one example, a lithium iron phosphate compound and a metal compound may have a molar ratio of about 1: 0.001-0.1. The cathode material can be doped with carbon additives distributed over grain boundaries or covering the grain surface. Alloying carbon additives can give the final cathode material with 1-15% carbon by weight. A carbon additive may include one or more components selected from the group consisting of carbon black, acetylene black, graphite, and a carbohydrate compound.

- 5 022170

The complex compound may include a lithium source, an iron source, a phosphate source, and a second crystalline compound with a molar ratio L: Pe: P: crystalline compound of about 1: 1: 1: 0.001-0.1. In other examples, other molar ratios of Li: Pe: P: crystalline compound may be used. The lithium source may include one or more components selected from the group consisting of lithium carbonate, lithium hydroxide, lithium oxalate, lithium acetate, lithium fluoride, lithium chloride, lithium bromide, lithium iodide and lithium dihydrogen phosphate. The iron source may include one or more components selected from the group consisting of iron oxalate (11), iron acetate (11), iron chloride (11), iron sulfate (11), iron phosphate (11), iron oxide (11) , iron oxide (111), complex iron oxide and iron phosphate (111). The phosphate source may include one or more components selected from the group consisting of ammonium, ammonium phosphate, ammonium dihydrogen phosphate, iron phosphate (11), iron phosphate (111), and lithium hydrogen phosphate.

A method for producing a mixed crystalline lithium iron phosphate cathode material involves mixing at least one HEPEO ₄ compound with a complex compound and heating the resulting mixture to 600-900 ° C in an inert gas or reducing gas atmosphere for about 2-48 hours. The complex compound may include two or more metal oxides in which the metal can be selected from the groups ΙΑ, ΙΙΑ, ΙΙΙΑ, 1УЛ, УЛ, ΙΙΙΒ, 1УВ and УВ of the Periodic table. The complex compound provides a mixed crystalline structure, the method of obtaining a complex compound with the corresponding mixed crystalline structure involves mixing metal oxides of groups ΙΑ, ΙΙΑ, ΙΙΙΑ, ΙνΑ, UL, ΙΙΙΒ, ΙΥΒ and HC and heating the mixture to 600-1200 ° C for 2 -48 hours

One way to obtain a mixed crystalline material of the cathode involves uniformly mixing sources of lithium, iron and phosphate and heating them to 600-900 ° C in an atmosphere of inert gas or reducing gas for at least about 2 hours. The resulting mixture can then be combined with the mixed a metal compound containing a combination of two or more metal oxides selected from the groups ΙΑ, ΙΙΑ, ΙΙΙΑ, [UD. YΑ, ΙΙΙΒ, ΙΥΒ and HC of the Periodic Table. In one embodiment, a lithium source, an iron source, a phosphate source and a mixed metal compound are capable of providing molar ratios L: Pe: P: mixed metal compound of 1: 1: 1: 0.001-0.1. In other embodiments, other molar ratios of Ы: Pe: P: mixed metal compound may be used. In addition, at least one carbon source may be added to the resulting mixture, this carbon source including one or more of the following components, without limitation: carbon black, acetylene black, graphite and a carbohydrate compound. The amount of carbon source added to the resulting mixture should provide the final product with a carbon content of 1-15% by weight.

The lithium source used to form the cathode material may include one or more of the following compounds, without limitation: lithium carbonate, lithium hydroxide, lithium oxalate, lithium acetate, lithium fluoride, lithium chloride, lithium bromide, lithium iodide and lithium dihydrogen phosphate. An iron source includes one or more of the following components, without limitation: iron oxalate (P), iron acetate (P), iron chloride (P), iron sulfate (P), iron phosphate, iron oxide (P), iron oxide ( Ш), complex iron oxide and iron phosphate (Ш). When a ferric compound is used as an iron source, the ball mill grinding process may include the addition of a carbon source to reduce ferric iron to ferrous iron. Sources of phosphorus may include one or more of the following compounds, without limitation: ammonium, ammonium phosphate, ammonium dihydrogen phosphate, iron phosphate (P), iron phosphate (III), and lithium hydrogen phosphate.

During grinding in a ball mill, one or more solvents may be added, including ethanol, deionized water, and acetone. In other embodiments, other mixing media and solvents may be used. In addition to this, the mixture can be dried between 40-80 ° C or mixed until dry.

The types of inert gases that can be used include helium, neon, argon, krypton, xenon, radon, and nitrogen. In addition, reducing gases, including hydrogen and carbon monoxide, may also be included. Other suitable gases may also be used.

The cathode sheet 110 may be formed using a suspension of cathode material, which includes one of the above active cathode materials. A suspension of the cathode material can be formed by mixing a thickener, an active cathode material and a solvent. A thickener and a solvent are first mixed together to form a colloidal solution. The resulting colloidal solution, solvent residue and active material are mixed in a double planetary mixer. Part of the solvent, as well as the binder, is then fed to a planetary mixer for further mixing.

The colloidal solution, cathode active material and solvent can be mixed in a double planetary mixer in accordance with the indicated mixing sequence. IN

- 6 022170 in this case, the colloidal solution, the active material and the solvent can be mixed for about

3-5 minutes at a speed of approximately 2-20 Hz, which is reduced to a lower speed of approximately 0-2 Hz. Then the colloidal solution, the active material and the solvent can be mixed for about 30-50 minutes at a speed in the range of about

35-60 Hz, which is reduced to a lower speed in the range of about 35-60 Hz. At this time, a vacuum can be created in the twin planetary mixer for about 3-5 minutes, so that mixing occurs at a pressure of from about 0.0005 to about

0.05 MPa. Then, residual solvent and adhesives are added to the double planetary mixer and mixed for about 5-10 minutes at a speed of about 35-60 Hz, which decreases to a lower speed in the range of about 35-60 Hz. Again, a vacuum can be created in the double planetary mixer for about 3-5 minutes, so that mixing takes place at a pressure of from about 0.0005 to about 0.05 MPa. Mixing takes place over about 20-35 minutes at a speed that decreases from about 10-25 to about 0 Hz.

The proportion by weight of the active material of the cathode, thickener, adhesives and solvent can be approximately 100: (0.05-10) :( 0.01-10) :( 50-150). The proportion by weight of solvent mixed with the thickener may be about 60-90%. When mixed with a colloidal solution and active material, the proportion by weight of solvent may be about 0.1-30% and may be about

8-20% when a binder is added.

The cathode sheet 110 may be formed by coating a suspension of an electrically conductive substrate, such as aluminum foil. The suspension may be applied to the electrically conductive substrate by a roll method, although other methods may be used. The electrical conductive substrate and the suspension are then dried to form a cathode sheet 110. The cathode sheet 110 preferably has a thickness in the range between 100 and 110 μm, although other thicknesses can also be used.

The separator sheet 115 may be a microporous polypropylene and / or polyethylene electrolytic membrane. Such membranes are available from I8 Ce1datb οί CHaNoIs. ΝοΠίι SatNia.

Referring again to FIG. 1, the anode sheet 105 includes a region in which the substrate 107 of the anode sheet 105 does not include active anode layers 106. In contrast, the copper substrate 107 is open to facilitate electrical connection with the anode sheet 105. The open area of the substrate 107 extends substantially along the entire length the anode sheet 105 so that the first edge of the anode sheet 105 defines the conductive region 107 when the battery sheet 100 is wound to form a wound core 200 (see Fig. 2). The open area of the substrate 107 can be formed by limiting the area on which the active anode layers 106 are deposited on the substrate 107. In addition, or alternatively, the open area of the substrate 107 can be formed after applying the active anode layers 106 by selectively removing the active anode layers 106 from the substrate 107 along a predetermined width of the anode sheet 105. This removal can be performed using a mechanical removal method and / or a chemical removal method.

The cathode sheet 110 includes a region in which the substrate 114 of the cathode sheet 110 does not include active cathode layers 112. In contrast, the aluminum substrate 112 is open to facilitate electrical connection with the cathode sheet 110. The open area of the substrate 112 extends substantially along the entire length of the cathode sheet 110 such that the edge of the cathode sheet 110 defines the conductive region 114 when the battery sheet 100 is wound to form a wound core 200 of FIG. 2A. The open area of the substrate 114 can be formed by limiting the area on which the active cathode layers 112 are deposited on the substrate 114. In addition, or alternatively, the open area of the substrate 114 can be formed after applying the active cathode layers 112 by selectively removing the active cathode layers 112 from the substrate 114 along a predetermined width of the cathode sheet 110. This removal can be accomplished using a mechanical removal method and / or a chemical removal method.

As shown in FIG. 2A, the anode sheet 105, the cathode sheet 110, and the separator sheet 115 can be wound to form a wound core 200. The open substrate 114 forms a multilayer current collector structure for the cathode of the wound core 200, while the open substrate 107 forms a multilayer current collector structure for the wound core of the wound core anode 200. The current collector for the cathode and the current collector for the anode are located at opposite ends of the length of the core 200 and provide low resistance contacts that can

- 7 022170 to conduct a current of significant magnitude. The formation of current collectors on opposite sides of the wound core 200 also simplifies the manufacturing process.

Current collectors can be formed by several different methods. For example, current collectors may be formed solely from exposed substrate layers. In addition to this, or alternatively, current collectors can be formed by attaching a tape of electrically conductive material along the length of each of the anode and cathode sheets, respectively, before or after winding.

The outer layer of the wound core 200 may be an insulator. In one example, the separator sheet 115 is longer than the anode sheet 105 and the cathode sheet 110. As such, the anode sheet 105 and the cathode sheet 110 are limited during the winding operation before reaching the end of the separator sheet 115. The excess length of the separator 105 is then wound around the core 200 a predetermined number of times ( for example, two or more), forming the outer insulating layer 115. This design simplifies the manufacture of the core 200 and, in addition, increases the uniformity of the structure of the core.

After the wound core 200 is formed, the open layers of the anode substrate 107 and the cathode substrate 114 are compressed to change their shape so that the external cross-sectional area of each end portion of the wound core 200 is smaller than the internal cross-sectional area of the core 200. For this, the open layers of the anode the substrates 107 of the wound core 200 may be welded to one another, bonded to one another by a mechanical fastener and / or bonded to one another using glue or the like. Preferably, the exposed layers of the anode substrate 107 are joined to one another by mutual compression, welding them together along the entire length or length sections of the open substrate 107, forming a monolithic structure of the anode current collector. The layers of the cathode substrate 114 can be formed in the same manner as the layers of the anode substrate 107.

An alternative structure for core 200 is shown in FIG. 2Β-2Ό. In this embodiment, a plurality of anode sheets, cathode sheets, and separator sheets are layered on top of one another. However, unlike the previously described core structure, the sheets forming the core are not wound into a roll. In contrast, the core 200 comprises a plurality of flat sheets, for example, as shown in the layout of FIG. 2B. Preferably, the end sheets of the core 200 are sheets of insulating material, and more preferably one or more separator sheets 115. A top view of this embodiment of the core 200 is shown in FIG. 2C, while a side view is shown in FIG. 2Ό. As illustrated, the layers of insulating material / separator preferably extend beyond the side edges of the stacked cathode and anode sheets and can be wrapped around the side edges to isolate the cathode and anode sheets from one another. Alternative methods of sealing packaged cathode and anode sheets may also be applied to prevent their unwanted mutual contact and to prevent environmental exposure. Although the current collectors 114 and 107 in FIG. 2B-2I are formed from the substrate layers of the anode and cathode sheet material, they can also be formed in the form of tapes that are connected to the individual stacked layers of the substrate.

FIG. 3 shows a perspective view of the anode end of a battery cell 300 having a wound core 200 (not shown, but implied in FIG. 3). In FIG. 3, the battery cell 300 includes a protective shell 305 in which a wound core 200 is housed. A current collector 310 is electrically connected to the first end 320 of the connecting structure 325 through the end cap assembly 335. The other end 330 of the connecting structure 325 extends through the corresponding cover plate / end cap 335. to provide external contact for the anode of the battery cell 300.

As shown in FIG. 3, the containment shell 305 is rectangular in shape and dimensioned such that the core 200 fits snugly into its interior. Although the sheath 305 (and the core 200 as such) may have different sizes, the protective sheath 305 may have a width V and a height H, with V greater than about 50 mm and H greater than about 100 mm. Preferably, the ratio between the width and height of the shell 305 corresponds to the following equation:

0.18 <ν / Η <0.5.

This ratio is also applicable in order to determine the overall dimensions of the core 200, and is particularly suitable when the battery cell 300 has a large capacity and high output power.

If the ratio ν / Η is greater than 0.5, then the width of the battery cell 300 is very large, and the total surface area of the shell 305 may not be able to withstand the pressure generated in its internal space, which causes its destruction and / or deformation. This may pose a security / reliability risk. If the ν / Η ratio is less than 0.18, then the height of the battery cell 300 is very small, so that the battery cell 300 is very thin. Available volume available to accommodate core 200

- 8 022170 inside the containment shell 305, is relatively small and unfavorable for accommodating a core with high capacity and high current.

FIG. 4 is a schematic cross-sectional view of a battery cell 300. In this example, the connecting structure 325 includes an angular connector 405, which extends through the cover plate / end cap 335. In this case, the angular connector 405 is essentially Ζ-shaped. The current collector 310 may be formed in the manner described above. For simplicity, the current collector 310 of FIG. 4 illustrates only a single strip of the anode current collector. A flexible connecting part 410 electrically connects the corner connector 405 to the current collector 310. The flexible connecting part 410 may include many layers of metal foil, such as copper, which are annealed and welded to both the angular connector and the current collector 310. A similar method can be used to connect the cathode current collector with corresponding angular connector of connecting structure. However, the flexible connecting part between the corner connector and the cathode current collector can be formed of several layers of aluminum foil that are annealed and welded to both the corner connector and the cathode current collector. The use of this type of interconnect structure facilitates the production of a battery using a wound core 200. In addition, the interconnect structure can be used to provide a low electrical resistance path for a large current to flow through the battery. Moreover, this structure can be applied to dissipate heat, which contributes to battery safety.

FIG. 5 and 6 show one of the methods for forming regions of the anode sheet 105 and / or the cathode sheet 110 that are adjacent to the open substrates 107 and / or 114, respectively. Only the region adjacent to the open substrate 107 is described, although the corresponding region adjacent to the open substrate 114 may have the same basic structure.

In FIG. 5 and 6, the anode sheet 105 has a total width of 505. The active layers 106 of the anode sheet 105 are applied across a width of 510 sheets, leaving an uncoated area having a width of 515. Alternatively, the uncoated area can be formed by removing part of the active component of the anode sheet 105. Coating from the active component gradually becomes thinner at the edge of the sheet over a width of 520. In the area to the left of the area 520, layers 106 are formed at their full thickness. Thinning starts at 525, transitional with respect to coating thickness. An insulating layer or coating is applied along area 530. The width of the layer (coated with insulating coatings) completely covers the portion with decreasing coating thickness on the electrically conductive substrate and ends in the portion with the electrically conductive substrate open. The layer / coating must be non-conductive in electrons and / or ions and able to maintain its integrity at high temperatures. One such coating is polyphenylene sulfide (PP8). Using this configuration reduces the possibility of a short circuit between the anode and cathode. In addition, thinning the coating in the manner described reduces the formation of wrinkles, which otherwise might occur during roll pressing of the coating having a thick edge.

FIG. 7 is a cross-sectional view of one example of a wound core 200. In a wound core, varying thicknesses of the core 200 and / or forces exerted thereon on opposing regions A and B can cause problems. In order to limit such problems, the anode sheet 105 and the cathode sheet 110 end on opposite arcuate regions C and вместо, instead of ending on opposite plane regions A and B. As shown in FIG. 7, the anode sheet 105 ends at a location 705 of the region C, while the cathode sheet 110 ends at a location 710 of the region Ό. The separator sheet 115 extends beyond the end locations 705 and 710 so that it is wound to form the outer part of the core 200. The separator sheet 115 ends at 715 along the arched side of the core 200. The direction in which the sheets are wound to form the core 200 is indicated by an arrow 720. In this structure, the cathode sheet 110 may be longer than the anode sheet 105.

In accordance with the design of the core 200 shown in FIG. 7, regions A and B are substantially flat and do not have significant thickness changes. As a result, there is a reduction in the formation of wrinkles that would otherwise form due to the swelling of the core 200 during the electrolyte impregnation, as well as during charging and discharging of the battery cell. Such wrinkles are formed when the forces acting on the core 200 in regions A and B are substantially uneven. By reducing the formation of wrinkles, the life of the core can be increased. Likewise, hidden security problems due to uneven charging or discharging of the core 200 are resolved (for example, situations in which the wrinkled portion of the core 200 creates lithium dendrites that cause a short circuit inside the battery resulting in an explosion).

FIG. 8 illustrates one embodiment of a bent connector 800 that can be used in the connecting structure 325 of FIG. 4. Curved connector 800 is formed of an electrically conductive material that is suitable for making an electrical connection as well as mechanically bonding with the material used to form the connector 410 of FIG. 4, and preferably has a width of at least 25% of the width of the protective sheath 305. The bent connector 800 of FIG. 8 is typically Ζ-shaped and includes a first part 805 and a second part 810, which extend in opposite directions from the transverse part 815. The second part 810, as will be described below, extends from the inner side of the battery cell to its outer side, where it connected to the transverse part 815. The transverse part 815 is located on the outside of the battery cell, where it electrically connects the second part 810 to the first part 805. The first part 805 actually forms the electrical terminal of the battery, which It can be used for access to an anode (or a cathode) wound around the core 200.

The bent connector 800 may include a weakening structure, such as a groove 820, which causes the electrical connection of the bent connector 800 to the core 200 to break under certain excessive forces, such as those that occur when the vehicle is involved in an accident. In FIG. 8, a single groove 820 extends substantially along the width of the transverse member 820. In addition or alternatively, the groove 820 may extend along the length of the first portion 805 from the outside of the battery cell 300 and / or along a portion of the second portion 810 from the outer side of the cell 300 batteries. Several attenuating structures may also be used.

Depending on the electrical resistance characteristics of the material forming the bent connector 800, the groove 820 may increase the resistance in an undesirable manner. In such cases, the groove 820 may be filled with an electrically conductive material that is mechanically plastic. Examples of materials suitable for this purpose include, but are not limited to, tin, conductive rubber, and other conductive plastic materials. The electrical resistance of the section with the groove 820 is thereby reduced, while the overall safety characteristic for which the groove is intended remains.

FIG. 9 illustrates another embodiment of a bent connector 900 that can be applied to the connection structure 325 of FIG. 4. The bent connector 900 is formed of an electrically conductive material that is suitable for creating an electrical connection as well as mechanically bonding with the material used to form the connector 410 of FIG. 4. The bent connector 900 of FIG. 9 is generally L-shaped and includes a portion 910 that extends from the inner side of the battery cell to its outer side, where it is connected to the transverse portion 915. The transverse portion 915 is located on the outside of the battery cell. The transverse portion 915 actually forms the electrical terminal of the battery, which can be used to access the anode (or cathode) of the wound core 200.

The bent connector 900 may include a weakening structure, such as a groove 920, which causes the electrical connection of the bent connector 900 to break in the area of the weakening structure. More specifically, the bent connector 900 breaks its electrical connection with the core 200 when subjected to certain excessive forces, such as those that occur when the vehicle is involved in an accident / collision. In FIG. 9, a single groove 920 extends substantially along the width of the transverse member 915. In addition or alternatively, the groove 820 may extend along the length of the portion 910 in a portion of the portion 910 that is external to the battery cell 300. Several attenuating structures may also be used.

Depending on the electrical resistance characteristics of the material forming the bent connector 900, the groove 920 may increase the resistance in an undesirable manner. In such cases, the groove 920 may be filled with an electrically conductive material that is mechanically plastic. Examples of materials suitable for this purpose include, but are not limited to, tin, conductive rubber, and other conductive plastic materials. The electrical resistance of the section with the groove 920 is thereby reduced, while the overall safety characteristic for which the groove is intended remains.

The dimensions of the grooves 820 and 920 of the curved connectors 800 and 900 depend on the material used to form the connectors 800 and 900. If the curved connector is formed of copper, then the depth of the corresponding groove can be 50-90% of the thickness of the transverse part. The width of the groove along the transverse part may be approximately 100-500% of the depth of the groove. If the bent connector is formed of aluminum, the depth of the corresponding groove may be 30-80% of the thickness of the transverse part. The width of the groove along the transverse part may be approximately 100-300% of the depth of the groove.

FIG. 10 shows how the bent connector of FIG. 8 can be used to interconnect adjacent battery cells. As shown element

- 10 022170

A battery 300a is located adjacent to the battery cell 300b for connecting them to one another. The battery cell 300a includes an end cap 335a. The curved cathode connector 800a extends from the inside of the battery cell 300a in which it is electrically connected to a cathode current collector of a corresponding wound core (not shown). The transverse portion 815a of the bent connector 800a extends toward the adjacent battery cell 300b. Similarly, the battery cell 300b includes an end cap 335b. The curved anode connector 800L extends from the inside of the battery cell 300B in which it is electrically connected to the anode current collector of the corresponding wound core (not shown). The transverse portion 815b of the bent connector 800B extends toward the adjacent battery cell 300a.

The surfaces of the upwardly directed portions of the connectors 800a and 800b are connected to one another at the junction 1005. The joint 1005 can be formed by welding the surfaces of one with the other, joining the surfaces of one with the other using glue such as electrically conductive rubber, mechanically interconnecting the surfaces of one with the other a fixture or similar structure and / or connection method. By interconnecting the curved connectors 800a and 800b on the surfaces of the upwardly directed parts between the cathode of the battery cell 300a and the anode of the battery cell 300b, a low electrical resistance connection is established through which a large current can pass. A similar structure can be applied at the opposite end of each battery cell 300a and 300b to provide a low electrical resistance connection capable of passing a large current between the anode of the battery cell 300a and the cathode of the battery cell 300b, with other neighboring cells, thereby connecting all elements 300 to each other. Thus, the neighboring battery cells are electrically connected in series with each other. However, this interconnect architecture can also be applied to electrically connect adjacent battery cells in parallel with each other.

Both bent connectors 800a and 800b include respective attenuation grooves 820a and 820b. If one or both of the battery cells 300a and / or 300b deviate from their respective positions due to an accidental collision with the vehicle, then the material in the region of the grooves 820a and / or 820b will be destroyed, which will cause electrical disconnection of the battery cells 300a and 300b from one another . The safety of the battery used in the vehicle is thus increased.

FIG. 11 shows another structure for interconnecting adjacent battery cells 300a and 300b. The interconnection is essentially the same as shown in FIG. 10. However, the bent connectors 800a and 800b are connected to one another using a fusible element 1105 placed between the surfaces of the upwardly directed parts. The fusible element 1105 may be tin-lead solder or similar material that melts and / or evaporates at excessively high currents / high temperatures that may occur if a battery cell 300a, a battery cell 300b, and / or a battery device including cells fail 300a and 300b of the battery. In this case, the thickness, width, length and composition of the fusible element 1105 are selected so as to provide electrical separation of the bent connectors 800a and 800L when the electric current and / or temperature between them exceeds a predetermined critical value. The safety of the battery cells 300a and 300b when excessive current and / or temperature conditions are present is improved by applying this interconnect structure.

FIG. 35 and 36 show a different interconnecting structure of adjacent battery cells 300a and 300b. As shown, the connecting structure includes a first curved connector 800a and a second curved connector 800b. Each bent connector 800a, 800b includes a first portion 810a, 810b, a transverse portion 815a, 815b, and a second portion 805a, 805b. In the embodiment shown in FIG. 35 and 36, parts 805a and 805b are shorter than the corresponding parts of the connectors shown, for example, in FIG. 8, 10 and 11. Curved connectors 800a and 800b can be connected to one another using a fusible element 1105 located between the surfaces of parts 805a and 805b. The fusible element 1105 may be tin-lead solder or similar material that melts and / or evaporates at excessively high currents / high temperatures that may occur if a battery cell 300a, a battery cell 300b, and / or a battery device including cells fail 300a and 300b of the battery. In this case, the thickness, width, length and composition of the fusible element 1105 are selected so as to provide electrical separation of the bent connectors 800a and 800L when the electric current and / or temperature between them exceeds a predetermined critical value. The safety of the battery cells 300a and 300b when excessive current and / or temperature conditions are present is improved by the use of

- 11 022170 of this interconnect architecture.

The connectors 800a, 800b can also be adapted to separate from one another when the interconnection structure is subjected to excessive forces that may occur, for example, when a vehicle is hit. For this, each transverse portion 815a, 815b includes a tapered section 3505a and 3505b. As shown, the tapered sections 3505a and 3505b define the open areas 3520. The open areas 3520 weaken the interconnect structure to facilitate disconnection of the connectors 800a and 800B under excessive loads. Each part 805a and 805b may have a width that is substantially the same or otherwise corresponding to the width of the tapered sections 3505a and 3505b.

FIG. 37 shows another structure for interconnecting adjacent battery cells 300a and 300b. This interconnect structure is similar to the interconnect structure shown in FIG. 36 and 37. However, portions 805a and 805b extend towards the battery cells 300a and 300b.

FIG. 38 shows another structure for interconnecting adjacent battery cells 300a and 300b. In this interconnect structure, the first curved connector 3800a extends from the battery cell 300a, while the second curved connector 3800b extends from the battery cell 300b. Each connector 3800a, 3800b includes a first portion 3805a, 3805b, which extends from a respective battery cell 300a, 300b and is connected to a corresponding second portion 3810a, 3810b. Parts 3810a and 3810b extend to one another and overlap one another in the area of connection 3815. Parts 3810a and 3810b can be adapted to separate one from the other when subjected to excessive forces, such as those arising from a collision of a vehicle. For this, one or both of the parts 3810a and 3810b may include a weakening structure. In FIG. 38, the weakening structure comprises narrowed sections 3820a and 3820b formed on superposed portions of parts 3810a and 3810b superimposed on one another. The tapered sections 3820a and 3820b may be formed as arcuate regions, similar to the connecting structures shown in FIG. 35-37.

FIG. 39 shows another structure for interconnecting adjacent battery cells 300a and 300b. In this interconnect structure, the first curved connector 3900a extends from the battery cell 300a, while the second curved connector 3900b extends from the battery cell 300b. Each connector 3900a, 3900b includes a first portion 3905a, 3905b, which extends from a respective battery cell 300a, 300b and is connected to a corresponding second portion 3910a, 3910b. Parts 3910a and 3910b extend towards one another and are connected end-to-end in connection region 3915. Connection region 3915 may include a generally U-shaped region that connects parts 3810a and 3810b using material that melts and / or evaporates at temperatures which occur when the current flowing between the elements 300a and 300b becomes excessively large.

The material in the connection region 3915 may be, for example, tin solder or other material capable of mechanically and electrically connecting the parts and, at the same time, melting and / or vaporizing at a desired overcurrent temperature. Each connecting portion 3900a, 3900b may include a weakening structure, such as a groove 920 on the connector 900 shown in FIG. nine.

FIG. 40 and 41 illustrate other interconnection structures, including mechanically weakened regions, which break the electrical connection between the elements 300a and 300b at a predetermined location when subjected to excessive forces that occur, for example, in a vehicle accident / collision. In FIG. 40, the connector 4005a is connected to the battery cell 300a, while the connector 4005b is connected to the battery cell 300b. The transverse portions 4000a and 4000b terminate in corresponding arcuate portions 4010a and 4010b that are connected to each other in the connection region 4015. The arcuate regions 4010a and 4010b are strong enough to provide mechanical and electrical connection between connectors 4005a and 4005b under normal operating conditions. However, the thinning of these areas of the material creates a weakened connecting structure in which the connection between the transverse elements 4000a and 4000b breaks due to the forces that occur during an accident / collision of a vehicle.

In FIG. 41, the connector 4105a is connected to the battery cell 300a, while the connector 4100b is connected to the battery cell 300b. The transverse parts 4100a and 4100b are stacked one on top of another in a region 4110, in which the connectors 4105a and 4105b are mechanically and electrically connected to one another. Each transverse portion 4100a, 4100b includes a corresponding arcuate region 4115a, 4115b in which the material forming the transverse portion is thinned. The transverse parts 4100a and 4100b are aligned in such a way that the arcuate regions 4115a and 4115b overlap one another in the connection region 4110. The resulting

- 12 022170 the structure is strong enough to facilitate mechanical and electrical connection between connectors 4105a and 4105b under normal operating conditions. However, the thinning of the material in the arcuate regions 4115a and 4115b creates a weakened connecting structure in which the connection between the transverse elements 4100a and 4100b breaks due to the forces that occur during an accident / collision of a vehicle.

FIG. 41A is a cross-sectional view of terminals 4100a and 4100b along secant 41A-41A in FIG. 41. In FIG. 41A, however, the multilayer clamp 4120 is positioned to clamp the arcuate regions 4115a and 4115b. Clamp 4120 includes a first layer 4125 and a second layer 4130 having different thermal expansion characteristics. In this case, the first layer 4125 may be an insulating material and have a higher coefficient of thermal expansion than the second layer 4130. With excessive current, the temperature of the terminals 4100a and 4100b increases. As the temperature increases, the first layer 4125 expands to a greater extent than the second layer 4130. Since the expansion of the first layer 4125 is limited to the second layer 4130, the first layer 4125 acts on thinned sections of material in the arcuate regions 4115a and 4115b. Finally, if the temperature exceeds a predetermined threshold value corresponding to excessive current, then the first layer 4125 applies a force to the arcuate regions 4115a and 4115b to interrupt the connection between terminals 4100a and 4100b.

FIG. 42-46 show various methods by which the terminals 4200a and 4200b of adjacent battery cells 300a and 300b can be connected to one another. Β In each case, the terminals 4200a, 4200b are connected to each other using an electrically conductive bridge connector 4205. The bridge connector 4205 may have a different shape, including, but not limited to, an I-shape, an inverted I-shape, an Ζ shape, a δ shape a shape or any other shape with one or more bending angles between about 0 and 180 °. The bridge connector 4205 may be formed as a single layer metal structure, a multilayer structure, or as a multilayer metal foil. The formation of the bridge connector 4205 in the form of a multilayer metal foil allows the bridge connector 4205 to additionally function as a mechanical buffer that absorbs vibration energy between the terminals 4200a and 4200b, thereby increasing the integrity of the overall design of the connection of the terminals.

The bridge connector 4205 may be formed from a single metal material, sheets of several metals with different coefficients of thermal expansion, and / or from a shape memory alloy. Examples of materials having different thermal expansion coefficients that can be used in a multi-metal sheet structure include a combination of Fe-листов sheets, a combination of Fe-Cu sheets and / or a combination of shape memory alloys / conventional metal. Shape memory alloys that can be used in bridge connector 4205 include Cu-based alloys and / or Fe-based alloys. These alloys include, without limitation, Cu-Ζη-ΑΙ,

Cu-Αί-Νί and / or Re-Μη. A common metal may be, for example, Cu, Α1 and / or Νί.

A bridge connector 4205 connects portions of terminals 4200a and 4200b facing one another. The effective welding surface of the bridge connector 4205 and the corresponding terminal may be about 0.5-4 of the terminal cross-sectional area. Solder having a lower melting point than the metal of the connector and the output can be placed at the junction of each end of the bridge connector 4205 and the corresponding output. The connection between each terminal and bridge connector 4205 may be formed by cold pressure welding, ultrasonic welding, solder welding, flash butt welding, friction welding, electrical contact welding, or the like. Preferably, the joint is formed by welding with solder at which the melting point of the alloy used as the solder is in the range between about 150 and 250 ° C. Materials that can be used include δη, Au-20% δη, lead-5% δη, H-δη, etc.

FIG. 42 shows a bridge connector 4205 having an inverted I-shape. In this embodiment, the leads 4200a and 4200b may share the characteristics of the leads 800a and 800b shown in FIG. 10. The bridge connector 4205 may include first and second parts 4210 and 4215, which are connected to one another by the transverse element 4220. The first part 4210 is connected to the output element 4225 4200a, while the second part 4215 is connected to the element 4230 output 4200b. The bridge connector 4205 may be formed as a multilayer soft metal part, for example, of a multilayer copper foil. If the battery cells 300a and / or 300b are exposed to external forces, the transverse cell 4220 can absorb the generated shock loads and protect the leads from excessive wear and damage.

The bridge connector 4205 may be formed from a shape memory alloy or a bimetal element. If the temperature of the interconnect structure suddenly rises due to, for example, excessive current or other abnormal conditions, the shape memory alloy or bimetallic element can be compressed in the direction shown by arrows 4235 to bring it out of contact with each of the terminals when the solder between the bridge / output connections melts. As a result, the electrical and mechanical connection between the terminals 4200a and 4200b is broken, preventing the explosion of the battery cells and / or other such dangerous consequences.

Shape memory alloys that can be used to make the 4205 bridge connector include Cu-based metal alloys and / or Fe-based metal alloys such as Cu-Ζη, Cu-Ζη-ΑΙ, Cu-ΆΙ-Νί, or Pe alloys -Μη-δί. With respect to the structure shown in FIG. 42, it is believed that a Cu-ΆΙ-сплав alloy is used. In such cases, the bridge connector 4205 may be initially formed so that the angle between each part 4210 and 4215 and the transverse element 4220 is less than 90 °. In this case, the bridge connector 4205 can be subjected to high temperature processing in the range of about 300-1000 ° C for several minutes to give a memory effect. The bridge connector 4205 then connects to pins 4200a and 4200b in the normal assembly position. In this position, the angle between each part 4210 and 4215 is approximately 90 ° with respect to the transverse element 4220. The shape memory alloy will tend to restore its original shape when the temperature of the bridge connector 4205 rises to a temperature corresponding to excessive current and / or another abnormal the operating condition of the battery cell.

FIG. 43 shows a bridge connector 4205 having a δ shape. In this embodiment, the leads 4200a and 4200b may share the characteristics of the leads 800a and 800b shown in FIG. 10. The bridge connector 4205 may include first and second parts 4305 and 4310, which extend in opposite directions and are connected to one another by the transverse element 4315. The first part 4305 is connected to the output element 4225 4200a, while the second part 4310 is connected to the element 4230 pin 4200b. As indicated above, the bridge connector 4205 may be formed of a multilayer metal foil, a bimetal element and / or a shape memory alloy. When forming from a shape-memory alloy, the bridge connector 4205 may have an initial shape that corresponds to the shape required to disconnect from terminals 4200a and 4200b at elevated temperatures that occur under excessive current and / or other abnormal operating conditions of the battery cell.

FIG. 44 shows a bridge connector 4205 having an inverted I-shape. In this embodiment, the leads 4200a and 4200b may share the characteristics of the leads 800a and 800b shown in FIG. 10. The bridge connector 4205 may include first and second parts 4405 and 4410, which are connected to one another by the transverse element 4415. The first part 4405 is connected to the outer surface of the output element 4225 4200a, while the second part 4410 is connected to the external surface of the output element 4230 4200b. As indicated above, the bridge connector 4205 may be formed of a multilayer metal foil, a bimetal element and / or a shape memory alloy. When forming from a shape-memory alloy, the bridge connector 4205 may have an initial shape that corresponds to the shape required to disconnect from terminals 4200a and 4200b at elevated temperatures that occur under excessive current and / or other abnormal operating conditions of the battery cell. In FIG. 44, the initial shape can be defined so that the bridge connector 4205 expands in the directions indicated by arrows 4420 at such elevated temperatures.

FIG. 45 shows a bridge connector 4205 having a multilayer structure. In this embodiment, the bridge connector 4205 includes a first layer 4505, which is located on the inside of the parts 4225 and 4230, and a second layer 4510, which is located on the inside of the first layer 4505 and has the same extent. Each layer 4505, 4510 has an inverted I-shape. Layer 4510 may be formed from ordinary metal, while layer 4505 may be formed from shape memory alloy. The conventional metal layer 4510 and the shape memory alloy layer 4505 may be connected to one another such that changes in shape of the shape memory alloy layer 4505 lead to corresponding changes in the shape of the conventional metal layer 4510. As such, the bridge connector 4205 changes shape at elevated temperatures that occur during excessive current and / or other abnormal operating conditions of the battery cell. This change in shape causes the bridge connector 4205 to disconnect from terminals 4200a and 4200b.

FIG. 46 shows a bridge connector 4205 having a multilayer structure. In this embodiment, the bridge connector 4205 includes a first layer 4605, which is located on the outside of the parts 4225 and 4230, and a second layer 4610, which is located on the outside of the first layer 4605 and has the same extent. Each layer 4505, 4510 has an inverted I-shape. Layers 4610 and 4605 are formed from metals having

- 14 022170 different coefficients of thermal expansion, and can be mechanically connected to one another so that a change in the shape of one layer will lead to a corresponding change in the shape of the other layer. The difference in the thermal expansion coefficients causes a change in the shape of the bridge connector 4205 at elevated temperatures that occur when excessive current and / or other abnormal operating conditions of the battery cell occur, whereby the terminals 4200a and 42006 are disconnected from each other. In order to further ensure that the leads 4225 and 4230 are electrically isolated from each other when the bridge connector 4205 changes shape, an insulating layer 4615 can be placed at the end portion of each of the parts 4225 and 4230 adjacent to the bridge connector 4205.

The interconnections of the battery cells, such as those shown in FIG. 39 may include structures for protection against excessive temperature by gravity. An example of one of these structures is shown in FIG. 47 and 48, with FIG. 47 is a plan view of the structure, and FIG. 48 is a side view of the structure. These figures show the orientation of the terminals when the battery cells are rotated to their sides in the manner shown in FIG. 28A and 69 below.

In the embodiment shown in FIG. 47 and 48, terminal 3900a is electrically connected to battery member 300a, while terminal 39006 is electrically connected to battery member 3006. The electrical conductive unit 4705 is connected to the ends of each of the terminals 3900a and 39006 using the connecting material 4710. The electrical conductive unit 4705 extends along the entire width of 4805 of the connectors 3900a and 39006, as well as along the entire thickness of 4715. The connecting material 4710 may be a δη based solder, a solder on Βί -based or Ζη -based solder, however, δη -based solder is preferred. In one example, the solder may have a thickness between about 0.3 and 1 mm, and preferably between about 0.5 and 0.8 mm. The melting point of the solder may be between about 100 and 450 ° C. If the melting point is too low, then the structure of the mutual connection may be unstable under normal operating conditions. If it is too high, then the melting point may not be reached under abnormal conditions with excessive temperature. Δη based solder is preferred since it has a melting point of about 231.9 ° C.

- 15 022170

The electrical conductive unit 4705 may be formed of a high density metal having a melting point that is at least about 50 ° C higher than the melting temperature of the connecting material 4710. Thus, the electrical conductive unit 4705 can be reliably connected to the terminals 3900a and 3900b using a suitable soldering method. Such methods may include soldering with induction heating, soldering with a soldering iron, soldering welding with contact heating, or similar bonding methods.

As shown in FIG. 48, the conductive unit 4705 may have a trapezoidal shape in which the base portion 4810 is located at the bottom of the connecting structure. The conductive unit 4705 is subjected to gravity in the direction shown by arrow 4815. If the connection structure is exposed to excessive temperature conditions, such as those created by excessive current or other abnormal operation of the battery device, then the connecting material 4710 begins to melt. When the connecting material melts, the conductive block 4705 moves downward in the direction 4815 under the influence of gravity. Ultimately, the conductive block 4705 disengages from the terminals 3900a and 3900b, whereby the electrical and mechanical connection between them is broken.

The interconnections of the battery cells may also include over temperature protection structures using electrical insulators that are dimensioned so as to expand the connection between the terminals when the temperature of the inter connection becomes excessively high. FIG. 49-51 illustrate three embodiments of such reciprocal compounds. In FIG. 49, the terminals 4900a and 4900b are connected to each other by means of a connecting material 4710. The connecting material 4710 may be a δη-based solder, a основе-based solder or a Ζη-based solder, however, a δη-based solder is preferred. In one example, the solder may have a thickness between about 0.3 and 1 mm. The melting point of the solder may be between about 100 and 450 ° C, and preferably is about 232 ° C. At the junction between terminals 4900a and 4900b, an expandable member 4905 is housed. As shown, the expandable member 4905 may have a circular cross-section, but other cross-sectional shapes may be used. In addition, the expandable element 4905 may be formed of an insulating material with a large coefficient of thermal expansion. In addition, the material forming the expandable member 4905 may have a melting point that is substantially higher than the melting point of the connecting material 4710.

When the interconnect structure is exposed to excessive temperature, the joint material 4710 begins to melt. In addition, the expandable member 4905 expands, parting parts 4910a and 4910b from one another. The characteristics of the connecting material 4710, the expanding element 4905 and the gap between the parts 4910a, 4910b are such that the expansion of the expanding element 4905 divides the parts 4910a and 4910b from one another to a distance sufficient to overcome the surface tension of the molten connecting material 4710. The connecting material 4710 flows out from the junction between the terminals and actually breaks the electrical connection between the elements of the battery.

The interconnection shown in FIG. 50, similar to that shown in FIG. 49. The fundamental difference between them is in the form of conclusions 5000a and 5000b. More specifically, terminals 5000a and 5000b include inwardly extending portions 5005a and 5005b, as opposed to outwardly extending portions 4910a and 4910b of terminals 4900a and 4900b.

The interconnect structure shown in FIG. 51 is similar to those shown in FIG. 49 and 50. The fundamental difference between them lies in the form of conclusions. More specifically, the interconnection shown in FIG. 51 includes an outlet 4900a having an outwardly extending portion 4910a that is electrically connected to an inwardly extending portion 5005b of an outlet 5000b. The electrical insulating element 5105 can be placed between the end of the terminal 4910a of the terminal 4900a and the transverse terminal 5110 of the terminal 5000. The electric insulation element 5105 helps to ensure that the terminals 4900a and 5000b are electrically disconnected from each other when the connecting material 4710 melts and flows from the junction between the parts 4910a and 5005b.

As described above, the interconnect structures may include connecting material between the terminals, which melts at the excessively high temperatures that occur due to the excessive current between the battery cells 300a and 300b. In addition, or alternatively, the interconnect structures may be provided with substructures releasing chemicals that interact with the joint between the terminals so that the terminals are mechanically and electrically separated from one another at such an excessively high temperature. FIG. 52 and 53 show examples of these substructures as applied to the interconnect structures shown in FIG. 40 and 41, respectively.

In FIG. 52, the connector 4005a is connected to the battery cell 300a, while the connector 4005b is connected to the battery cell 300b. The transverse parts 4000a and 4000b end with the corresponding arcuate sections 4010a and 4010b, which

- 16 022170 connected to each other in the area of connection 4015. The area of connection 4015 may include a connecting material, such as solder. The arcuate regions 4010a and 4010b are strong enough to provide a mechanical and electrical connection between connectors 4005a and 4005b under normal operating conditions. However, the thinning of these areas of the material creates a weakened connecting structure in which the connection between the transverse elements 4000a and 4000b breaks due to the forces that occur during an accident / collision of a vehicle.

One embodiment of a chemical releasing substructure that interacts with the 4015 region of the compound is shown generally as 5205. In this embodiment, the 5205 substructure includes an outer shell 5210 in which the chemically reactive material 5215 is housed. Shell 5210 has a generally round cross section and adapted to fit inside the arcuate areas 4010a and 4010b. Other cross-sectional shapes may also be used, depending on the particular design of the leads used. Sheath material must meet several requirements. For example, the sheath material should be capable of binding to materials of parts 4005a and 4005b. In addition, the shell material should not react with the chemically reactive material 5215. In addition, the temperature at which the shell material begins to melt should be close to the temperature created by excessive current. The sheath material may be synthetic resin, rubber, ceramic, or the like. Preferably, the shell is formed of plastic and / or rubber compound with a melting point between 100 and 350 ° C, depending on the requirements for excessive temperature. Such materials may include ΡΡ, ΡΕ, ΑΒδ, ΡΡΟ, ΡΡδ, ΡΤΕΕ and ΡΕΕΚ.

The chemically reactive material 5215 is preferably a liquid at an overcurrent temperature. It may or may not be solid at normal operating temperatures. For example, it may be a solution of an acidic or alkaline chemical that reacts with the material in the region of compound 4015. Preferably, the chemical is an alkaline chemical, including, for example, ΝαΟΗ.

Under normal conditions, the temperature of the parts 4000a and 4000b is below the melting point of any material in the interconnect region 4015, and also below the melting temperature of the shell 5210 of the chemically reactive element 5205. When the temperature rises due to, for example, excessive current, the shell 5210 begins to melt. When the shell 5210 melts, the chemically reactive material 5215 is released and comes into contact with the materials of parts 4000a and 4000b, as well as any material in the reciprocal bonding region 4015. The released chemical reacts with the material in the interconnect region 4015, part 4000a and / or part 4000b. The reaction is destructive and leads to the electrical separation of parts 4000a and 4000b from one another.

In FIG. 53, the connector 4105a is connected to the battery cell 300a, while the connector 4100b is connected to the battery cell 300b. The transverse parts 4100a and 4100b are stacked one on top of another in a region 4110, in which the connectors 4105a and 4105b are mechanically and electrically connected to one another. Each transverse portion 4100a, 4100b includes a corresponding arcuate region 4115a, 4115b in which the material forming the transverse portion is thinned. The transverse parts 4100a and 4100b are aligned so that the arcuate regions 4115a and 4115b overlap one another in the connection region 4110. The resulting structure is strong enough to facilitate mechanical and electrical connection between the connectors 4105a and 4105b under normal operating conditions. However, the thinning of the material in the arcuate regions 4115a and 4115b creates a weakened connecting structure in which the connection between the transverse elements 4100a and 4100b breaks due to the forces that occur during an accident / collision of a vehicle.

As in FIG. 52, the interconnect structure of FIG. 53 includes a substructure 5205 that can release chemicals interacting with the region of compound 4110 under conditions of excessive temperature / excessive current. Substructure 5205 includes an outer sheath 5210, which contains chemically reactive material 5215. Sheath 5210 may have a generally circular cross section and is adapted to fit within the arcuate regions 4115a and 4115b. The action of substructure 5205 with respect to region 4110 is essentially the same as that described in connection with FIG. 52.

The interconnect structures shown in FIG. 52 and 53 are based on the horizontal alignment of the parts of the terminals connecting the battery cells 300a and 300b.

However, it should be appreciated that a substructure of the type that is generally shown as 5205 can be applied to other orientations of the interconnect structure. With these alternative orientations, substructure 5205 is designed and aligned with the leads so that reactive material 5215 is released, interrupting the electrical connection between the leads. Moreover, substructure 5205 can be located on only one of the terminals in order to interrupt the electrical connection between the terminals.

Overcurrent protection can be based on removing the conductive fluid between the terminals of the battery cells 300a and 300b. More specifically, the electrically conductive liquid is between the terminals of the cells 300a and 300b of the battery under normal operating conditions, so that the terminals are electrically connected to one another by passing an electric current. The conductive fluid is removed from the space between the terminals of the battery cells 300a and 300b when the temperature of the terminals rises due to, for example, excessive current or other device malfunction.

FIG. 54 shows one embodiment of an overcurrent protection substructure based on this principle. In this embodiment, terminal 5400a is connected to battery member 300a, and terminal 5400b is connected to battery member 300b. The terminals 5400a and 5400b are mechanically separated from one another in the separation region 5403. The electrical connection between the terminals 5400a and 5400b is established using the interconnect substructure 5405. The interconnect substructure 5405 includes a sheath 5410 in which the liquid conductor 5415 is held. The liquid conductor 5415 creates an electrical connection between the terminals 5400a and 5400b in the region 5403. As the liquid conductor 5415, metals, metal alloys, and electrically conductive solutions can be used. Preferably, the liquid conductor 5415 is mercury or an Να-сплав alloy. Shell 5405 has a generally circular cross-section, but other cross-sectional shapes may be used, depending on the particular design of the leads used. The sheath material may be non-reactive with respect to the liquid conductor 5415. In addition, the temperature at which the sheath material begins to melt should be close to the temperature created by excessive current. The sheath material may be synthetic resin, rubber, ceramic, or the like. Preferably, the shell is formed of plastic and / or rubber compound with a melting point between 100 and 350 ° C, depending on the requirements for excessive temperature. Such materials may include PP, PE, AB8, PPO, PP8, PTE and PEEK.

Under normal conditions, the temperature of the parts 5400a and 5400b is lower than the melting temperature of the sheath 5410, and the liquid conductor 5415 is held in the region 5403, facilitating current flow between the terminals 5400a and 5400b. When the temperature rises due to, for example, excessive current, the sheath 5410 begins to melt. When the sheath 5410 melts, the liquid conductor 5415 is released from the sheath 5410 and the open circular region 5403. Further current flow between the battery cells 300a and 300b through the terminals 5400a and 5400b stops.

FIG. 55-57B show another embodiment of an interconnect structure in which overcurrent protection is based on removing electrically conductive liquid between the terminals of the battery cells 300a and 300b. In this embodiment, the overcurrent protection substructure, shown generally as 5500, is configured to function with terminals that extend horizontally from each battery cell. As shown, terminal 5400a is connected to and extends horizontally from the battery cell 300a. The terminal 5400b is connected to the battery cell 300b and extends horizontally from it. Each terminal 5400a and 5400b extends from a respective battery cell into a conductive chamber 5505 of the overcurrent protection substructure 5500. Under the conductive chamber 5505 there is a drain chamber 5510. The conductive chamber 5505 and the drain chamber 5510 are made of an insulating material such as plastic, rubber, ceramic or the like. During normal operation of the battery device, the conductive chamber 5505 and the drain chamber 5510 are sealed so as to prevent leakage from one chamber to another.

Protection substructure 5500 can be assembled in a number of different ways. FIG. 56 shows one such method. In FIG. 56, substructure 5500 is formed of two parts 5600a and 5600b. Part 5600a is connected to terminal 5400a and sealed with it. Part 5600b is connected to terminal 5400b and sealed with it. Each part 5600a and 5600b includes half of the conductive chamber 5505 and half of the drain chamber 5510. Parts 5600a and 5600b can be connected to one another using hot-melt sealant, rubber, adhesive, welded or the like. Parts 5600a and 5600b can be sealed together with the corresponding terminals 5400a and 5400b using injection molding, hot-melt sealant, adhesive bonding, sealing with penetrating agents, or the like. The method used to connect the parts to one another and to the leads should be efficient enough to prevent any leakage of fluid from the conductive chamber 5505 or the waste chamber 5510.

FIG. 57A and 57B are cross-sectional views of a protection substructure 5500 during normal battery operation. During normal operation, a liquid conductor 5415 of the type described above is contained within the conductive chamber 5505 and creates an electrical connection between terminal 5400a and terminal 5400b. A fluid conductor 5415 may be introduced into the conductive

- 18 022170 chamber 5505 through a hole 5515 located in the upper part of the conductive chamber 5505. After filling the conductive chamber 5505 with the required amount of liquid conductor 5415, the hole 5515 may be closed by a plug or other type of seal.

The conductive chamber 5505 is separated from the drain chamber 5510 to prevent leakage of the liquid conductor 5415 from the conductive chamber 5505 to the drain chamber 5510. FIG. 57B shows one of the methods for separating the conductive chamber 5505 from the drain chamber 5510. In this example, the conductive chamber 5505 ends with a bottom wall 5705 that separates the conductive chamber 5505 from the drain chamber 5510. The lower wall 5705 of the chamber includes a flow opening 5715 that is normally sealed with a separation element 5720. The separation element 5720 may be made of plastic and / or rubber material having a melting point between about 100 and 350 ° C, depending on the desired temperature at which The overcurrent protection must be activated. Suitable materials include, for example, PP, PE, ΛΒδ, PPO, ΡΡδ, PTPE and / or PEEK.

With excessive current / battery failure, the temperature of the liquid conductor 5415 will increase. When the temperature reaches the melting temperature of the separation element 5720, the separation element 5720 will not allow the conductive chamber 5505 to separate from the drain chamber 5510. The liquid conductor 5415 will flow from the conductivity chamber 5505 to the drain chamber 5510 through the flow hole 5715. The flow may occur due to gravity and / or under the action of the force created by the increased pressure in the conductive chamber 5505 (for example, the force created due to the increased temperature of the liquid conductor 5415 with excessive current ) When the liquid conductor 5415 is discharged from the conductive chamber 5505, it will create an open circuit state between the terminals 5400a and 5400b. In order for the entire liquid conductor 5415 to be discharged from the conductive chamber 5505, the volume of the drain chamber 5510 must be at least equal to or greater than the volume of the conductive chamber 5505.

Protection substructure 5500 can be easily fabricated and easily repaired / reused. By collecting the liquid conductor 5415 in the waste chamber 5510, it is possible to reuse it in a repaired or new protection substructure 5500. This is especially useful if the 5415 liquid conductor is harmful to the environment. In addition, the protection substructure 5500 can be easily repaired by directing the liquid conductor 5415 back into the conductive chamber 5505 and replacing the sealing member 5720.

FIG. 58-60 show another embodiment of an interconnect structure in which overcurrent protection is based on removing electrically conductive fluid between the terminals of the battery cells 300a and 300b. In this embodiment, the overcurrent protection substructure, shown generally as 5800, is configured to function together with leads that extend horizontally from each battery cell. As shown, terminal 5800a is connected to and extends in a vertical direction from the battery cell 300a. The terminal 5800b is connected to the battery cell 300b and extends vertically from it. Each terminal 5800a and 5800b extends from a respective battery cell into the conductive chamber 5805 of the overcurrent protection substructure 5800. A drain chamber 5810 is located under the conductive chamber 5805. The conductive chamber 5805 and the drain chamber 5810 are made of non-conductive material such as plastic, rubber, ceramic, or the like. During normal operation of the battery device, the conductive chamber 5805 and the drain chamber 5810 are sealed so as to prevent leakage from one chamber to another.

Protection substructure 5800 can be assembled in a number of different ways. FIG. 59 shows one such method. In FIG. 59, substructure 5800 is formed of two parts 5900a and 5900b. Part 5900a is connected to terminal 5900a and sealed with it. Part 5900b is connected to terminal 5800b and sealed with it. Each part 5900a and 5900b includes half of the conductive chamber 5805 and half of the drain chamber 5810. Parts 5900a and 5900b can be connected to one another using hot-melt sealant, rubber bonding, adhesive bonding, weld bonding, or the like. In addition, parts 5900a and 5900b can be sealed together with the corresponding terminals 5800a and 5800b using injection molding, hot-melt sealant, adhesive bonding, sealing with a penetrating agent, or the like. The methods used to connect the parts to one another and to the terminals must be effective enough to prevent leakage of fluid from the conductive chamber 5805 or waste chamber 5810.

FIG. 60 is a cross-sectional view of a protection substructure 5800. During normal operation, a liquid conductor 5415 of the type described above is contained within the conductive chamber 5805 and creates an electrical connection between terminal 5800a and terminal 5800b. The liquid conductor 5415 may be introduced into the conductive chamber 5805 through a hole 5815 located at the top of the conductive chamber 5805. After filling the conductive chamber 5805 with the required amount of liquid conductor 5415, the hole 5815 may be closed by a plug or other type of seal.

- 19 022170

The conductive chamber 5805 is separated from the drain chamber 5810 to prevent the liquid conductor 5415 from leaking from the conductive chamber 5805 to the drain chamber 5810. In FIG. 60, the conductive chamber 5805 ends with a lower wall 6005 that separates the conductive chamber 5805 from the drain chamber 5810. The lower wall 6005 of the chamber includes a flow hole 6015, which is normally sealed with a spacer 6020. The spacer 6020 may be made of plastic and / or rubber material having a melting point between about 100 and 350 ° C., depending on the desired temperature at which overcurrent protection should be activated. Suitable materials include, for example, PP, PE, ΆΒδ, PPO, PP8, PTE and / or PEEK.

With excessive current / battery failure, the temperature of the liquid conductor 5415 will increase. When the temperature reaches the melting temperature of the separation element 6020, the separation element 6020 will not allow the conductive chamber 5805 to separate from the drain chamber 5810. The liquid conductor 5415 will flow from the conductive chamber 5805 to the drain chamber 5810 through the flow opening 6015. The flow may occur due to gravity and / or under the action of the force created by increased pressure in the conductive chamber 5805 (for example, the force created due to the increased temperature of the liquid conductor 5415 with excessive current ) When the liquid conductor 5415 is discharged from the conductive chamber 5805, it will create an open circuit state between terminals 5800a and 58006. In order for the entire liquid conductor 5415 to be discharged from the conductive chamber 5805, the volume of the drain chamber 5810 must be at least equal to or more than the volume of the conductive chamber 5805.

FIG. 12 and 13 show a connection structure 1200 that can be used to bring the core of the battery cell 300 to the optimum operating temperature when the ambient temperature drops below a predetermined threshold value. The connecting structure 1200 includes a heating element 1205, such as a ceramic heater, that is mounted on a bent connector 800. Between the bent connector 800 and the heating element 1205, a layer of heat-conducting material 1210 is placed. The heating element 1205 may have an L-shaped cross section and be dimensioned so that correspond to the surface of the bent connector 800, the opposite of the surface used to establish electrical connection with the neighboring element of the battery. Layer 1210 may be formed from a material, such as heat-conducting rubber, which serves as a heat-conducting element, an electrical insulator, and / or as an adhesive between the heating element 1205 and the curved connector 800. In addition, or alternatively, the curved connector 800 and the heating element 1205 can be connected to one another using a mechanical fastener that is made of an insulating material such as PA66.

FIG. 13 shows a device that can be used to increase the temperature of the core of a battery cell 300 when temperature conditions indicate that the core is at a predetermined threshold temperature or may drop below it. As shown, the device includes a temperature sensor 1305, which is positioned to monitor the temperature associated with the need of the core for heating. The temperature sensor 1305 may be arranged so as to monitor the ambient temperature of the vehicle, the ambient temperature of the battery device, the temperature of the battery cell 300 and / or other desired temperature. Temperature information is provided to the control system 1310. The control system 1310 uses information from the temperature sensor to determine when the temperature detected by the sensor 1305 falls below a predetermined threshold value. If this happens, the control system 1310 directs the electric power to the heating element 1205. The electric power can be provided by a generator associated with the gas engine of the vehicle and / or the battery system. The heating element 1205 responds to the supplied electric power by generating heat, which is transmitted through the layer 1210 to the bent connector 800. The bent connector 800, in turn, acts as a heat-conducting element that transfers heat to the interior of the battery cell 300, thereby raising the temperature wound core 200.

FIG. 14A shows one of the methods for connecting the structure 1450 to the multiple cores of the battery cell 300 with a curved connector 800. In this embodiment, the multi-core structure 1450 includes three separate cores, each of which is constructed in the same manner as the core 200. For simplicity, shown only one end of the battery cell 300, although the same basic structure can be used to connect the opposite end of the multi-core structure 1450 with corresponding m end connector 800.

In FIG. 14A, a multi-core structure 1450 is placed inside a rectangular protective sheath 305. An end cap assembly 335 is connected to an opening at the end of the sheath 305

- 20 022170 and seals it. A gasket 1405 formed of an insulating material is placed inside the shell 305 and is located between the end of the multi-core structure 1450 and the end cap assembly 335. The bent connector 800 extends into the interior of the battery shell 305 through the end cap assembly 335 so that it is offset from the middle a line extending in the longitudinal direction through the sheath 305.

A top view of the gasket 1405 is shown in FIG. 15. The gasket 1405 has three holes 1505, 1510 and 1515. Each hole is defined by a corresponding set of contour elements located on each side of the hole. Hole 1505 is defined by contour elements 1520 and 1525, hole 1510 by contour elements 1525 and 1530, and hole 1515 by contour elements 1530 and 1535. Each contour element includes a rounded surface on the side closest to the wound core 200 and a corresponding flat surface opposite to the rounded surface. The contour elements 1525 and 1530 are spaced apart so that the hole 1510 is larger than the holes 1515 and 1520. As a result, the flat surface of the contour element 1525 is positioned so as to protect the core 200 in the event that the bent connector 800 is biased towards the core 200 under the influence of excessive forces that may occur in a collision of a vehicle.

With reference again to FIG. 14A, current collector strips 1415 extend from the anode (or cathode) of each core 200 of the multi-core structure 1450. Each current collector strip 1415 may be formed from one or more foil layers, such as foil layers forming the anode (or cathode) substrate layers of each core 200. Although each current collector strip 1415 is shown as a single foil layer, each current collector strip 1415 may also be formed from several layers of foil that are grouped one upon the other when they extend from the anode (or cathode) of each core 200 of the multi-core structure 1450. In FIG. 14A, there are three current collector strips 1415a, 1415b, and 1415c that extend from the anode (or cathode) of the corresponding core 200 of the multi-core structure 1450. These current collector strips extend through respective openings 1505, 1510 and 1515 and into the cavity 1420 of the gasket 1405. Inside the cavity 1420, each current collector strip 1415a, 1415b and 1415c is electrically and mechanically connected to a corresponding flexible connecting foil 1425a, 1425b and 1425c. Various joining methods that can be used to join the structures include, but are not limited to, ultrasonic welding, electrical resistance welding, laser welding, and / or another joining method.

As shown in FIG. 14A, the connecting foils 1425a, 1425b, and 1425c are bent inside the cavity 1420 to be connected to the common side of the bent connector 800. The connecting foils 1425b and 1425c are bent inside the first side of the cavity 1420, while the connecting foil 1425a is curved inside the second side of the cavity 1420 The first side of the cavity 1420 is larger than the second side of the cavity 1420 due to the displacement of the connector 800 with respect to the longitudinal midline of the sheath 305. Therefore, the connecting foils 1425b and 1425c have more space in which they can be bent to attach to the connector 800 than the connecting foil 1425a. The angles at which the connecting foils 1425b and 1425c are bent are therefore relatively smooth. Smooth bending angles are more desirable than sharp bending angles and, to a lesser extent, lead to rupture of the corresponding connecting foil. However, the connecting foil 1425a is located in a smaller part of the cavity 1420. In this case, a sharper bending angle may be required for the connecting foil 1425a to bend the foil for connection with the connector 800. The sharp bending angles are subject to significant mechanical and thermal fatigue and can lead to rupture of the connecting foil 1425a.

In order to make the bending configuration of the connecting foil 1425a more reliable, an annular guiding element 1430 is connected to the connecting foil 1425a. The annular guiding element 1430 includes a connecting part 1435 and a rounded part 1440. The connecting part 1435 is connected to the connecting foil 1425a from the outside of its connection with other connecting foils 1425b and 1425c. The rounded portion 1440 has a shape and a diameter for bending the connecting foil 1425a with a smooth bending angle as it approaches the curved connector 800, thereby increasing the reliability of the connecting foil 1425a. In addition, the annular guide element 1430 may be sized to exert a pressing force on the current collector strip 1415a and the connecting foil 1425a toward the side of the gasket 1405. As a result, the current collector strip 1415a and the connecting foil 1425a do not undergo such significant movement as it can otherwise occur when the cell 300 is exposed to vibration. Similarly, the lengths of the connecting foils 1425b and 1425c can be chosen so that an appropriate bending configuration limits the vibration of these components within the chamber 1420. The reliability and safety of the battery cell 300 is enhanced in the case of such structures.

The use of the annular guide element 1430 can be expanded to nodes having more than three connecting foils, as well as nodes having less than three connecting foils. In each case, the annular guide member 1430 is preferably attached to the connecting foil which bends on the side on which it is connected to the curved connector 800, as opposed to the connecting foil which is curved below and around the curved connector 800 for connection. In addition, additional annular guide elements can be bonded to the connecting foils 1425b and 1425c to prevent unnecessary bending of these connecting foils as well.

FIG. 14B shows one of the methods for connecting the core of the battery cell 300 to the curved connector 800. In this embodiment, only one single core 200 is used. Accordingly, only one current collector 1415 extends from the core 200 for electrical connection with the curved connector 800. In order to reduce the sharpness of the corners, formed in the connecting foil 1425 to achieve the curved connector 800, the current collector 1415 is passed through the hole 1515, which is located farthest from the curved connector 800. In in all other respects, the end cap 300 of FIG. 14B is the same as the cap shown in FIG. 14A.

The gasket 1405 may include tabs 1410 that engage with corresponding recesses in the sheath 305. The tabs 1410 may be used to secure the gasket 1405 to the sheath 305. In addition, or alternatively, the gasket 1405 may be secured within the sheath 305 by welding, one or more mechanical fasteners, glue or other connection mechanism.

Gasket 1405 helps protect core 200 in several different ways. For example, a portion of the gasket 1405 adjacent to the core 200 helps to maintain the core 200 in a longitudinal position in the interior of the containment shell 305. The offset of the contour element 1525 helps prevent the connector 800 and its lateral connections from touching the core 200 during an accident or mechanical damage. . The narrowing of the holes provided by the contour elements 1520, 1525, 1530, and 1535 helps guide the current collectors 1415a, 1415b, and 1415c to the chamber 1420 during the manufacture of the battery cell 300. In addition, the gasket 1405 contributes to an increase in the rigidity of the containment shell 305 to provide an increased degree of protection for the wound core 200.

FIG. 16 and 17 show one method of sealing the end of the containment 305 with the end cap assembly 325. FIG. 16 is a cross-sectional sectional view of the end cap assembly 325, and FIG. 17 is a longitudinal sectional view of an end cap assembly 325.

The end cap assembly 325 includes a cover plate / end cap 1605, a hollow holder 1610, a connector 800, and a sealing material 1615. In order to make the end cap assembly 325, the cover plate 1605 and the hollow holder 1610 are welded together to form an integral structure. Without limitation, the welding operation may include laser welding, argon arc welding and other welding methods. Cover plate 1605 and hollow holder 1610 may be made of stainless steel. After welding the cover plate 1605 and the hollow holder 1610 with one another, they can be placed on the connector 800, which extends from the inside of the battery cell to the outside (out). The end cap assembly 325 includes a cover plate 1605, a hollow holder 1610, a connector 800, and sealing material 1615. In order to make the end cap assembly 325, the cover plate 1605 and the hollow holder 1610 are welded together to form an integral structure. Without limitation, the welding operation may include laser welding, argon arc welding and other welding methods. The technological operations that take place after the cover plate 1605 and the hollow holder 1610 are welded to each other are operations without intense heating. Therefore, the likelihood that other components of the battery cell will be damaged in the manufacture of the end cap assembly 325 is reduced.

Cover plate 1605 and hollow holder 1610 may be made of stainless steel. Before further processing the surface of the cover plate 1605, the hollow holder 1610 and the connector 800, which will be in contact with the sealing material 1615, can be sanded to increase the adhesion between these components and the sealing material 1615.

With reference to FIG. 16 and 17, connector 800 includes upper channels 1620 located on opposite sides of connector 800, and lower channels 1625 located on opposite sides of connector 800. Upper and lower channels 1620 and 1625 extend substantially along the length of connector 800. Channels 1620 are located such that they generally coincide with the inwardly extending protrusions 1630 of the hollow holder 1610.

- 22 022170

Connector 800 also includes a plurality of through holes 1635 that extend all the way across the entire width of the connector. As shown in FIG. 16, the through holes 1635 are located next to another set of inwardly extending protrusions 1640 of the hollow holder 1610. As shown in FIG. 17, the through holes 1635 may be located at different positions along the length of the connector 800 and between the channels 1620 and 1625.

After the cover plate 1605 and the hollow holder 1610 have been welded together, the connector 800 is guided to its desired position in the inner channel of the hollow holder 1610 and the sealing material 1615 is pumped into the intermediate regions between the connector 800, the hollow holder 1610 and the cover plate 1605. The sealing the material is injected under high pressure to fill the channels 1620, 1625, through holes 1635, and also the areas around the inwardly extending protrusions 1630 and 1640.

Sealing material 1615 may be plastic (e.g., PPA, ΡΕδ, ΡΡδ, modified PP, etc.), a rubber compound, a resin (e.g., an epoxy resin, a phenolic resin modified with an epoxy resin, etc.), an adhesive resin (e.g. two-component epoxy, hot-melt resin, etc.). Sealing material 1615 must be an electrical insulator and resistant to electrolyte and hydrochloric acid. In addition, the sealing material 1615 must be capable of bonding with various metals used to make the connector 800, the hollow holder 1610, and the cover plate 1605 (e.g., copper, aluminum, stainless steel, and other metals).

Sealing material 1615 extends beyond the top of the hollow holder 1610. More specifically, the sealing material 1615 fills the interior between the hollow holder 1610 and the connector 800 and covers the outside of the hollow holder 1610, forming a protective flange 1645. The protective flange 1645 also improves the integrity of the seal. In addition, the protective flange 1645 can to some extent absorb vibrational and shock forces that would otherwise affect the connector 800.

As shown in FIG. 61, the end cap assembly 325 may also include an additional protective cover 6105, which generally corresponds to the outermost parts of the other elements of the end cap assembly 325. In the illustrated embodiment, the protective cover 6105 includes a first portion 6115 that extends along and corresponds to the outer surface of the cover plate 1605 The cover plate 1605 may include a cover plate flange 6120 that is engaged with a corresponding flange 6125 of the first part 6115. The cover 6105 also includes a second part 6110, which extends at an angle, for example, of about 90 ° with respect to the first part 6115. The second part 6110 extends around and corresponds to the outer surface of the hollow holder 1610 and the protective flange 1645 and ends with an opening 6130 through which the outlet 800 protrudes. Preferably, the second part 6110 is sealed together with the outlet 800 at the hole 6130. In addition, the second part 6110 includes an inner flange 6140, which is engaged with the protective flange 1645. The area of the second part 6110 below the inner flange 6140 may be dimensioned so that the protective flange 1645 applies force e to the protective cover 6105, in order to facilitate the fastening of the protective cover 6105 to the cover plate 1605.

The protective cover 6105 may be formed of an insulating material. For example, the protective cover 6105 may be formed from plastic (e.g., RRL, ΡΕδ, modified PP, or the like), rubber (e.g., based on a copolymer of ethylene, propylene and diene monomer (EPOM), styrene butadiene rubber, or the like. n.), resin (epoxy modified with phenolic aldehyde epoxy or the like). Such materials are insulators, they are fire resistant and are difficult to degrade under the action of the electrolyte of the battery cell. By forming a protective cover 6105 using electrical insulating materials, the probability of short circuits due to physical deformation (for example, in a collision / accident of a vehicle) of the connector 800 with respect to the cover plate 1605 is reduced and eliminated. Similarly, the protective cover 6105 can extend around the edge sections of the cover plate 1605 to avoid unwanted electrical contact between the battery cell and other battery structures about the device.

The protective cover 6105 may be formed as a solid structure or composite structure. FIG. 62 and 63 illustrate the composite structures of the protective cover, while FIG. 64 illustrates the integral structure of the protective cover.

In FIG. 62, the protective cover 6105 is formed from two separate halves 6200a and 62006 of the protective cover. Each half of 6200a and 62006 includes a corresponding first part 6115a, 61156, which is dimensioned to extend along and corresponds to the outer surface of the cover plate 1605. Each half 6200a and 62006 also includes a corresponding flange 6125a, 61256, which is engaged with the corresponding flange 6120 of the cover plate . The second parts 6110a, 61106 extend at an angle, for example, of approximately 90 ° with respect to the first parts 6115a, 61156. The second parts 6110a, 61106 are dimensioned to extend around and correspond to the outer surface of the hollow holder 1610 and the protective flange 1645. Holes 6130a, 6130b are formed through each half of 6200a, 6200b and are sized to allow terminal 800 to protrude through them. The second portions 6110a, 6110b include inner flanges 6140a, 6140b, which are connected to the protective flange 1645. The protective flange 1645 may apply force to the inner flanges 6140a, 6140b to help secure the protective cover 6105 to the cover plate 1605.

Half of the protective cover 6200a, 6200b are connected to each other using mating structures. In FIG. 62, half 6200a includes a rectangular protrusion 6205a that is sized to fit into the rectangular hole 6205b of half 6200b. When a protective cover 6105 is applied to the end cap assembly 325, the halves of 6200a and 6200b can be directed laterally to one another so that the inner flanges 6140a and 6140b engage with the lower side of the protective flange 1645. At the same time, the mating structures 6205a and 6205b direct one to the other, until they are essentially or fully linked. Depending on the size and parameters of the protective cover 6105, a binding agent may be applied to the external surface of each of the mating structures 6205a and 6205b before assembly to increase the overall integrity of the protective cover 6105. Other bonding methods may also be used.

- 24 022170

The mating structures can take many forms. In FIG. 63, half 6200a includes an oval protrusion 6305a that is sized to engage with the corresponding oval hole 6305b of half 6200b. Other forms of mating structures may also be used (for example, triangular, trapezoidal or the like).

In FIG. 64, the protective cover 6105 is formed as a single integral structure. When fabricated in this way, the protective cover material preferably has high elasticity so that the protective cover can be applied to the end cap assembly 325 around the terminal 800.

The protective cover 6105 may include a means of visual indication indicating the characteristics of the battery cell / output. In the protective covers shown in FIG. 6264, a visual polarity indicator 6215 is provided to identify the corresponding terminal as a cathode terminal or anode terminal. Indicator 6215, by way of example, identifies the corresponding terminal 800 as a cathode terminal.

With reference to FIG. 17, the end cap assembly 325 includes a blow hole 1800. The blow hole 1800 is designed to prevent a catastrophic rupture of the battery cell 300 if the internal pressure of the battery cell 300 reaches a dangerous level. If this pressure is not relieved, the cell 300 may explode. In each of FIG. 62-64, the cover 6105 includes a vent 6210 that is located above the blow hole 1800 so that the cover does not interfere with the release of gases and / or other materials from the blow hole 1800.

FIG. 18 shows one embodiment of a blower assembly 1800 that can be used on the end cap assembly 325. The blower assembly 1800 includes a vent cover 1805, a tear pin 1810, and a vent base 1815. As shown, the blow assembly 1800 is mounted over the vent hole 1820 of the cover plate 1605 .

Vent cover 1805 may take the form of a truncated trapezoidal cone with an open side surface. A plurality of outlet openings 1825 are located on the sides of the vent cover 1805. The total area of the outlet holes 1825 should be larger than the area of the hole 1820. The tear pin 1810 extends through an opening at the top of the vent cover 1805 to which it is fastened, for example, by spot welding.

Vent base 1815, as shown in both FIGS. 18 and 19, includes a circular ring 1830 and a flange 1835. A deformable membrane 1840 is attached to the circular ring 1830 by welding it over the inner opening of the ring. The width of the circular ring 1830 is preferably less than about 70% of the width of its inner hole. In addition, the width of the protrusion 1845 of the circular ring 1830 preferably does not exceed 70-80% of the width of the ventilation hole 1820.

The deformable membrane 1840 is preferably formed from the same material as the cover plate 1605 (e.g., aluminum, stainless steel, etc.) and has a thickness in the range of about 0.01-0.1 mm, with a preferred thickness between 0.01 and 0.05 mm. The thickness of the deformable membrane 1840, however, can be changed in accordance with the level of excessive pressure at which the ventilation unit 1800 must collapse. The deformable membrane 1840 may be soldered to properly seal the opening of the circular ring 1830 from above, and may be formed of a metal foil such as aluminum foil, copper foil, and the like.

The ventilation base 1815 is welded to the cover plate 1605 using a high-energy beam, such as a laser or electron beam. Vent cover 1805 includes a spacer 1850 that is connected to vent base 1815. Spacer 1850 has several holes 1855 that are distributed around its circumference to facilitate high-energy beam welding of vent cover 1805 with vent base 1815.

When the pressure inside the battery cell 300 approaches a critical level, the deformable membrane 1840 deforms toward the breakaway pin 1810. When the critical pressure is reached, the deformed membrane 1840 breaks through the bursting pin 1810 to relieve pressure and prevent the battery cell 300 from exploding. The pressure at which the deformable membrane 1840 ruptures can be adjusted by adjusting the distance between the deformable membrane 1840 and the rupture pin 1810. In addition, the shape of the rupture pin 1810 can be used to cause different rupture modes at different critical pressures. Moreover, when during the assembly of the battery cell, air inside the battery cell 300 is consumed during the manufacturing process, a deformation of the deformable membrane 1840 occurs, which increases the distance between the membrane and the burst pin 1810. This property contributes to the rapid production of normal batteries and reliable removal of - 25 022170 normal batteries from the production line.

FIG. 21 and 22 show alternative pressure relief structures 2100 and 2200. Each structure may be sealed with a corresponding outlet of the cover plate 325. The pressure relief structure 2100 is formed from a deformable membrane 2105 having a weakening groove 2110. Similarly, the pressure relief structure 2200 is formed from a deformable membrane 2205 having a weakening groove 2210. The fundamental differences between structures 2100 and 2200 are in the shape formed by the edges of each membrane and the shape of the weakening groove located in each membrane. The dimensions of the deformable membranes 2105 and 2205 of each pressure relief structure 2100 and 2200, as well as the depth and length of each weakening groove 2110 and 2210, depend on the specific pressure at which the corresponding structure must collapse to prevent the battery cell from exploding. Another alternative pressure relief structure involves filling the vent with polymer sealing material, wherein the polymer seal is adapted to break above a predetermined pressure.

FIG. 65-67 illustrate another embodiment of a blow hole 1800. FIG. 65 shows the blow hole 1800 in an assembled state on the cover plate 1605. FIG. 66 is a perspective view of a blow hole 1800, while FIG. 67 is a cross-sectional view of a blow hole.

In this embodiment, the blow hole 1800 includes a membrane 6605, which is located in the recess 6610, which, in turn, surrounds the outlet 1820 of the cover plate 1605. The recess 6610 includes an inner edge 6625 defining the hole 1820 and an outer edge 6620 defining the periphery of the recess 6610. The distance in the radial direction between the edges 6620 and 6625 can be from about 10 to 15% of the radius of the outlet 1820.

The membrane 6605 is dimensioned to fit tightly into the space inside the outer edge 6620 of the recess 6610. Various materials that can be used to form the membrane 6605 include, for example, aluminum, aluminum alloy, steel, or any other material that meets the requirements for destruction of the material for the blow hole 1800. In addition, the material can be selected so that it can be easily welded. The thickness of the material may be between about 0.01 and 0.1 mm. Although the illustrated membrane 6605 is circular, other shapes (e.g., rectangular, elliptical, square or the like) may also be used.

A protective mask 6615 is placed over the membrane 6605. The protective mask 6615 includes a support ring 6630, which is tightly aligned with the outer edge 6620 of the recess 6610, while it is welded with the outer edge 6620 in one or more places 6705. Welding methods that can be applied include for example, laser welding and / or electron beam welding.

The upper part 6635 extends from the support ring 6630 in the direction from the membrane 6605. The upper part 6635 may have a radius, which is usually equal to the radius of the hole 1820. Several oval holes 6640 are located on the side walls of the upper part 6635. The total area of the oval holes 6640 may be approximately equal to or greater than the area of the hole 1820. The wall thickness of the protective mask 6615 may be in the range between about 0.1 and 0.5 mm.

The above blow hole structure can be applied to achieve numerous advantages. For example, assembling a structure is both simple and economical. When the membrane 6605 and the protective mask 6615 are assembled over the hole 1820, the assembly can be easily connected to the cover plate 1605 by welding the support ring 6630 of the protective mask 6615 with the outer edge 6620 of the recess 6610. The protective mask 6615 helps protect the membrane 6605 from external forces, thereby improving the overall integrity of the blow hole 1800. Moreover, a protective mask 6615 can be applied to reduce the release of non-gaseous materials from the battery cell when the internal pressure of the battery cell tarei exceeds safe levels.

FIG. 23 is a structural diagram of a battery 2300 in which several battery cells 300 are connected in series and grouped inside one housing 2305. The number of battery cells 300 in a single housing 2305 may range from 8 to 15, and a preferred number of cells in the battery is 10. Connectors 2810 conclusions are located on opposite ends of the battery 2300 and are used to provide means for creating electrical and mechanical soy Inonii several batteries 2300. The housing 2305 is preferably hermetically sealed and is waterproof, but includes channels 2310 for flow of coolant therethrough. Channels 2310 are located on the sides on opposite sides of the battery 2300 so that the coolant flows near the connectors 800 to heat or cool the cells 300 of the battery 2300.

- 26 022170

The protective shells of the neighboring battery cells can be adjacent to one another in such a way that they are in direct contact with one another or located directly adjacent to one another on opposite sides of the insulating sheet.

FIG. 24 is a perspective view of one embodiment of a housing 2305 that can be used to form a battery 2300. In this embodiment, housing 2305 includes a plurality of battery cells 300 connected in series. The battery cells 300 are connected to one another in the same manner as shown in FIG. 23. Between each element 300 of the battery is placed a separator 2405 made of insulating material to electrically isolate the protective shells of the elements 300 of the battery from one another. Preferably, however, separators 2405 are not used. In contrast, the containment shells are preferably in direct contact with one another, so that they form a single thermal unit. Temperature control is thereby maintained in a simpler manner.

The battery cells 300 are located between the lower plate 2410 and the upper plate 2415 to limit the movement of the battery cells 300 along the y axis. Partitions 2420 are located on each side of the group of battery cells 300 and are oriented across the length of the battery cells 300. Partitions 2420 act in conjunction with one another to limit the movement of the battery cells 300 along the x axis. Side plates 2425 are located at opposite ends of the battery cells 300 and extend across the width of the battery cell group. Side plates 2425 restrict the movement of the battery cells 300 along the ζ axis.

Sealing elements 2450 can be located between each baffle 2420 and the upper and lower plates 2415, 2410, as well as between each side plate 2425 and the upper and lower plates 2415, 2410. Thus, the upper and lower plates 2415, 2410 form a waterproof seal with mating components. Such seals help prevent short circuits that might otherwise occur when the battery cell 300 is damaged and fluid can flow out of it.

Partitions 2420 are made of insulating plastic material having the desired mechanical strength, resistance to thermal degradation, ductility at low temperature and resistance to chemicals in the battery and the environment in the vehicle. One embodiment of partition 2420 is shown in FIG. 25. Each septum structure 2420 includes a septum plate 2430, a septum stiffener 2435, and openings 2440 located at the corners of the septum structure 2420. Holes 2440 are adapted to receive respective tension rods that extend between the septa 2420 to hold the battery cells 300 together. The total thickness of each structure of the partition 2420 may be from about 3 to 15 mm. The thickness of each plate 2430 septum may be in the range between approximately 3 and 5 mm The thickness of each stiffener 2435 of the partition may be in the range between about 5 and 2 mm. The stiffening element 2435 of the septum evenly distributes horizontal and vertical forces throughout the structure of the septum 2420 and increases the ability of the structure of the septum 2420 to protect the cells 300 of the battery. Through holes can be pre-formed in proper positions to facilitate the use of mechanical fasteners, such as screws, at the four corners of the structure of the partition 2420. Such mechanical fasteners are suitable for connecting the upper and lower plates 2415, 2410 with the structure of the partition 2420. On the partition 2420 there are b-shaped structures that are positioned so that they mate with the upper and lower plates 2415, 2410. The upper plate 2415 is located between the upper b-shaped structure uroy and lower

A b-shaped structure of the septum 2420. The hole is located between the upper plate 2415 and the upper b-shaped structure of the septum 2420. The hole is adapted to receive a rod that restricts movement between the upper plate 2415 and the septum 2420, thereby restraining the movement of the battery cells 300 along the x axis and y axis.

The upper and lower plates 2415, 2410 are made of plastic insulating material having the desired mechanical and chemical characteristics. As shown in FIG. 26, each of the upper and lower plates 2415, 2410 comprises a flat plate 2605, a stiffener 2610 and holes 2615. Holes 2615 are adapted to receive respective tension rods that extend between the upper and lower plates 2415, 2410. The total thickness of each of the upper and lower plates 2415, 2410 may be between about 3 and 15 mm. The thickness of each flat plate 2605 may be between about 3 and 5 mm. The thickness of each stiffener 2610 may be between about 5 and 10 mm between. The stiffener 2610 is adapted to evenly distribute horizontal and vertical forces throughout the respective structures of the upper and lower plates 2415, 2410. Pre-embedded bolts on the upper and lower plates 2415, 2410 are used to connect the upper and lower plates 2415, 2410 with partitions 2420, as well as with side plates 2425. A spacer on the inside of the top plate 2410 restricts the movement of the battery cells 300 along the y axis.

Side plates 2410 are made of plastic insulating material having the desired mechanical and chemical characteristics. As shown in FIG. 26, each side plate 2425 has a contour that corresponds to side holes formed when the upper plate 2415 and the lower plate 2410 are connected to each other.

The battery case 2305 is beneficial for several reasons. For example, the battery case 2305 limits the movement of the battery cells 300 in any movement that exceeds normal, thereby increasing the reliability of the battery 2300 and increasing the battery life. The movement of the battery cells 300 can be easily limited along each axis by designing the partitions 2420 and the upper and lower plates 2415 so that the space occupied by the battery 2300 is reduced. As a result of the formation of the housing 2305 from the insulating material, the risk of short circuits is reduced since the cells 300 the battery cannot be in contact with each other through the housing 2305. In addition, through the use of plastic material to form the components of the housing and 2305 the mass of the battery 2300 is reduced. Moreover, the likelihood that short circuits will occur due to leakage of the battery cell is reduced, since the sealing material is placed at the joints between the various components of the battery 2300, thereby preventing leakage of liquid from the battery.

FIG. 27 shows a connector 2700 that is used to mechanically and electrically interconnect adjacent batteries 2300. The connector 2700 includes a first electrical conductive portion 2705 and a second electrical conductive portion 2710 that are connected by an arcuate laminated metal foil 2715. The arcuate foil 2715 may have a thickness between about 0.01 and 5.0 mm and can be formed from copper foil to make it weldable. Alternatively, the electrical conductive parts 2705 and 2710, as well as the arcuate foil 2715, may be formed from nickel, aluminum, or other metals. Preferably, the electrical conductive parts 2705, 2710 and the arcuate foil 2715 are made of the same material to increase the overall electrical conductivity of the connector 2700. The formation of the arcuate foil 2715 may include hot pressing of several thin metal sheets when connecting them to one another, along with molding them in the form arcuate structure. Each electrically conductive portion 2705 and 2710 includes an L-shaped joint 2720 adjacent to the arcuate foil 2715, on which the arcuate foil 2715 is welded and / or hot-pressed to the corresponding portion. The size of each electrically conductive part 2705, 2710 and the arcuate foil 2715 is determined by the size of the electrode leads of the batteries that use the connector 2700, as well as the required current carrying capacity between the batteries. The arcuate foil 2715 may be dimensioned so that it ruptures when exposed to a shock force that exceeds a predetermined amount, thereby disconnecting the battery from a neighboring battery. Moreover, the arcuate foil 2715 may be sized to function as a fuse to disconnect adjacent batteries when the current between adjacent batteries exceeds a predetermined level. FIG. 68 shows another connector 2700 that can be used to mechanically and electrically interconnect adjacent batteries 2300. In this embodiment, the connector 2700 includes a first conductive portion 6805 and a second conductive portion 6810, which are connected by an arcuate metal element 6815. An arcuate metal element 6815 may be formed into a metal mesh 6825 that extends between opposing arcuate support portions 6830. The metal mesh 6825 may Met thickness between about 0.01 and 5.0 mm and may be formed of metal threads one kind or more of metals to make it suitable for welding. Parts 6805, 6810 may be formed into metal sheets having openings 6820 through which fasteners extend to connect connector 2700 to respective batteries. The electrical conductive parts 6805 and 6810, as well as the arcuate metal element 6815, may be formed of copper, nickel, aluminum, or other metals. Preferably, the electrically conductive parts 6805, 6810 and the arcuate metal element 6815 are made of the same material in order to increase the overall conductivity of the connector 2700. The size of each electrically conductive part 6805, 6810 and the arcuate metal element 6815 is determined by the size of the electrode leads of the batteries,

- 28 022170 that use the 2700 connector, as well as the required current carrying capacity between the batteries. The arcuate metal element 6815 may be dimensioned so that it ruptures when exposed to a shock force that exceeds a predetermined amount, thereby disconnecting the battery from a neighboring battery. In addition, the metal element 6815 can be adapted to operate as a fuse for disconnecting adjacent batteries when the current between adjacent batteries exceeds a predetermined level. Moreover, the connector 2700 can be formed so that it is flexible enough to mechanically damp any movement between adjacent batteries.

FIG. Figure 28 shows how the connectors 2700 are used to interconnect multiple batteries 2805a and 2805b, which are located in a head-to-head configuration. However, the batteries 2805a and 2805b may also be located side by side, as shown in FIG. 69, and still use connectors 2700. As shown, each of the batteries 2805a and 2805b has a pair of battery terminals located on one side of the battery, one terminal on each end of that side. The battery terminals may be adapted to burst when subjected to excessive forces during a vehicle accident or the like. A 2700 connector is applied at each end of the battery to establish a mechanical as well as electrical connection between the battery terminals. For simplicity, only the terminals 2810a and 2810b are shown and described, although the same configuration is applied between each terminal of the battery that is adjacent to the terminal of another battery. A connector 2700 between the batteries 2805a and 2805b provides a mechanical buffer that absorbs shock forces when relative displacement occurs between the batteries 2805a and 2805b. Moreover, the connector 2700 may be adapted to break the connection between adjacent batteries when exposed to excessive forces that occur in a vehicle accident or the like.

The connector 2700 is attached to the batteries 2800a and 2800b by connecting the conductive portion 2710 to the connection plate 2830a of the terminal 2810a and the conductive part 2705 to the connection plate 2830b of the adjacent terminal 2810b. Each conductive portion 2705 and 2710 includes a groove 2725 adapted to receive a welding wire (see FIG. 27). In addition, each part 2705, 2710 includes a plurality of holes 2730 adapted to receive mechanical fasteners. To connect the adjacent terminals of the batteries 2805a and 2805b, a welding wire is placed in each groove 2725. Each part 2705, 2710 is then welded (for example, using soldering, laser welding, ultrasonic welding, etc.) with the corresponding output. Preferably, each part is connected to a respective terminal by soldering. The solders in a simple manner support the interconnection between the batteries and furthermore simplify the replacement of the battery in the battery device, since the metal alloy forming the interconnection can be easily re-heated to separate the battery from other batteries in the battery device. In addition, mechanical fasteners 2840, such as screws, bolts or the like, are inserted into the holes 2715 to connect the corresponding holes of the respective terminals and to establish a more reliable connection between the electrically conductive part and the corresponding terminal. Welding and connecting the 2700 connector to the corresponding terminals of adjacent batteries in this embodiment creates a path with a low resistance and a high allowable current between adjacent batteries. Although adjacent batteries may be connected in such a way that they are electrically parallel to one another, their preferred arrangement is a series connection.

FIG. 29 shows a battery device 2900 that supplies electric power to an engine / generator and receives electric power from an engine / generator of a vehicle capable of being driven by electric power. Battery device 2900 includes several batteries 2805. The number of batteries may be about five, and preferably ten. Each battery 2805 includes a plurality of cells 300, preferably in the interval between 8 and 15 cells, and more preferably ten cells. The cells 300 of each battery 2805 are electrically connected in series with one another. In addition, several batteries 2805 are electrically connected in series with one another.

Each battery 2805 is located in a respective battery case 2305. The vehicle is equipped with a compartment containing several batteries and their housing. The compartment facilitates electrical connection to the engine / generator. The battery case 2305 for each battery 2805 is substantially sealed against the environment (for example, it is waterproof),

- 29 022170 with the exception that holes are provided through each battery 2805 in an area adjacent to their respective terminals. The openings of the housings 2305 of adjacent batteries are interconnected by a channel functioning to facilitate the circulation of cooling fluid, such as air, through the battery device 2900.

The compartment containing the battery device 2900 may be shaped and dimensioned to be partially located under the rear passenger seat of the vehicle and partially in the trunk of the vehicle. Alternatively, the compartment may be shaped and sized to be placed under the vehicle floor.

In FIG. 29, a heat transfer medium, such as air, is passed through a 2900 battery device by a pump 2905. A pump 2905 passes a heat transfer fluid through a device 2900 in the directions indicated by arrows 2910. As illustrated by arrows, a 2905 pump directs heat transfer through a heat treatment section 2915 before being supplied to an input 2927 of a central channel 2930 for distribution to other parts of the device 2900. The heat treatment section 2915 may include a refrigerator 2920 to cool the coolant and a heater 2925 to heat the coolant. The refrigerator 2920 is driven when the temperature of the battery device 2900 exceeds a predetermined threshold value. Similarly, the heater 2925 is activated when the temperature of the battery device 2900 falls below a predetermined threshold value.

When the coolant circulates through the central channel 2930, it heats or cools the terminal sections of each battery 2805 adjacent to the central channel 2930. When the end portion 2940 of the channel is reached, the coolant is directed to the outer channels 2910, 2940 of the battery device 2900. This allows the coolant to heat or cool the sections the terminals of each battery 2805 adjacent to the external channels of the battery device 2900. The elements 300 of the battery inside the battery device 2900, thereby BID in a controlled environment in which the temperature is maintained at an optimum level. Part of the coolant may be directed from the channels of the battery device 2900 into the passenger compartment of the vehicle. Thus, the heat generated by the battery device 2900 is used to heat the interior of the passenger compartment of the vehicle. The amount of heat transferring from the channels of the battery device 2900 can be controlled by a person inside the passenger compartment in order to adjust the temperature of the compartment.

FIG. 30-34 illustrate the benefits of providing connections to the anode and cathode of a wound core at opposite ends of the core. For comparison, FIG. 30 shows a battery 3000 having a core 3005, an anode connector 3010 and a cathode connector 3115. An anode connector 3010 and a cathode connector 3015 are located on the same side of the core 3005. The current distribution in the core 3005 during operation is indicated by shading. As shown, there is a significant current density in the region adjacent to the connectors 3010 and 3015. The areas with high current density are areas with elevated temperature in accordance with Ohm's law. Therefore, the areas adjacent to the connectors 3010 and 3015 are heated during operation and degrade battery performance. It also affects the battery life of 3000.

FIG. 31 shows a battery 3100 having a wound core 3105, an anode connector 3110, and a cathode connector 3115. An anode connector 3110 and a cathode connector 3115 are located on opposite sides of the wound core 3105. The core 3105 has a length of 3120 and a width of 3125. The anode connector 3110 has a width of 3130, in while the cathode connector 3115 has a width of 3135. Although the width of 3130 and the width of 3135 are shown to be smaller than the width of 1025, these widths can be increased so that they are substantially commensurate with the width of 3125 of the core 3 105.

The dimensions shown in FIG. 31 may have various proportions. For example, the ratio of length 3120 to width 3125 may be in the range between about 1.5 and 4.5, preferably between about 2.5 and 3.5. The ratio of width 3130 to width 3135 may be in the range between about 0.8 and 1.2, preferably between 0.9 and 1. The ratio of width 3130 (as well as width 3135) and width 3125 may be in the range between about 0.3 and 0.6, preferably between 0.4 and 0.5.

FIG. 32 illustrates a case in which width 3130 and width 3135 are approximately the same. In this case, the electric field 3200 forms an angle θ with respect to the edge of the core 3105. The value of the angle θ is defined as 1ap ^-1 ((^ -a) / b), where is the width 3125; a - width 3130; B is the length of 3120. If the angle θ is in the range between about 0 and 20 °, then the current density can be optimized. This happens when 0 <(^ - a) / b <0.37.

FIG. 33 illustrates the current density in core 3105 during operation. As shown, the current density is not concentrated on one side of the core 3105, but rather distributed

- 30 022170 on opposite sides closest to the anode connector 3110 and the cathode connector 3115. The current density near the middle of the core 3105 is reduced compared to FIG. 30. Accordingly, the central part of the core 3105 does not undergo significant temperature increases. In addition, temperature changes do not concentrate on one side of the core 3105.

FIG. 34 is a table comparing the operating parameters of a battery constructed in accordance with FIG. 30 (denoted as battery A) with respect to a battery constructed in accordance with FIG. 31 (designated battery B). The columns in FIG. 34 correspond to the following values:

column 3405 shows the number of discharge / charge cycles for each battery;

column 3410 shows the battery capacity after the number of cycles shown in column 3405;

column 3415 shows the ratio of the current battery capacity to the original battery capacity after the number of cycles shown in column 3405;

column 3420 shows the maximum temperature near the anode connector that appears during battery operation after it has been subjected to the number of cycles shown in column 3405;

column 3425 shows the maximum temperature near the cathode connector that appears during battery operation after it has been subjected to the number of cycles shown in column 3405; and

- 31 022170 column 3430 shows the maximum temperature near the center of the core that appears during battery operation after it has been subjected to the number of cycles shown in column 3405.

As shown, there are significant differences between the operating parameters of battery A and battery Β. The differences in operating parameters increase markedly when the battery is subjected to more charge / discharge cycles. Therefore, the performance of battery Β improves over time compared to battery A, and battery Β has a longer life.

Although various embodiments of the present invention have been described, it will be apparent to those skilled in the art that various other embodiments and implementations are possible within the scope of this invention. Accordingly, the invention is not limited to anything other than the appended claims and their equivalents.

Claims (6)

CLAIM 1. A battery device for storing electric power and supplying electric power to a vehicle comprising a plurality of batteries, each battery comprising a plurality of cells, wherein the cells in each battery are electrically connected to each other within a corresponding battery, and batteries are electrically connected to each other in order to provide electrical power from the elements of a plurality of battery cells. batteries to the vehicle, and each element in each battery contains a curved connector with the first shoulder and the second shoulder, the second arms of each two adjacent elements extend towards each other and are brought together in the connection area so that the elements are electrically connected to each other, with This electrical connection, at least between some of the elements, includes a separable area provided in said connection area, whereby the electrical connection can be locally divided into this separable region under the influence of an impact force exceeding a predetermined value, as well as under the influence of excessive current / excessive temperature, for which the indicated separable region contains an overcurrent / excessive temperature protection element containing connecting material connecting the end portions of the respective second arms and used to facilitate electrical connection between at least some of the elements, and The bonding material has a melting point that corresponds to an excessive current / excessive temperature state between the elements, and the connecting material is released from an electrical connection having an element of protection against excessive current / excessive temperature when the connecting material melts. 2. The device according to claim 1, in which the element protection against excessive current / excessive temperature contains the first electrical output, electrically connected to the core of the first element and having a first connecting surface; the second electrical output electrically connected to the core of the second element and having a second connecting surface, wherein the connecting material facilitates the electrical connection between the first and second connecting surfaces of the first and second electrical terminals at their electrical interface. 3. The device according to claim 2, also containing an insulating part located at the electrical junction between the first and second connecting surfaces, the insulating part having a coefficient of thermal expansion at the melting temperature of the connecting material, sufficient to dilute the first and second connecting surfaces from each other, so that facilitate the removal of the connecting material from the space between the first and second connecting surfaces. 4. The device according to claim 3, in which the insulating part expands sufficiently at the melting temperature of the connecting material in order to overcome the surface tension of the molten connecting material on the first and second connecting surfaces. 5. The device according to claim 3, also containing a weight placed at the junction between the first and second connecting surfaces, which is removed from the junction under the action of gravity when the connecting material melts. 6. The device according to claim 5, in which the electrical connection between the first and second connecting surfaces comprises a first layer of connecting material between the first connecting surface and the first load side; - 32 022170 second layer of connecting material between the second connecting surface and the second side of the load, with the first and second layers of connecting material completely physically separated from one another by a load.